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Rockets (Aeronautics)

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Morphology of Propulsive Power (Pasadena, CA: Society for Morphological Research, 1962), by F. Zwicky (page images at HathiTrust)
Aerodynamics, Propulsion, Structures and Design Practice (Princeton, NJ et al.: D. Van Nostrand Co., c1956), by Everard Arthur Bonney, Maurice J. Zucrow, and C. W. Besserer (page images at HathiTrust)
Effect of throttling on interface behavior and liquid residuals in weightlessness / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Eugene P. Symons and Lewis Research Center (page images at HathiTrust)
Experimental investigation of the feasibility of ablation-cooling a rocket nozzle with possible application to solid-propellant engines / (Washington, D.C. : National Aeronautics and Space Administration, 1961), by Richard R. Cullom and Lewis Research Center (page images at HathiTrust)
The wind-induced loads on a dynamically scaled model of a large missile in launching position / (Washington, D.C. : National Aeronautics and Space Administration, 1959), by Donald A. Buell, George C. Kenyon, and Ames Research Center (page images at HathiTrust)
Opportunities for ballistic missions to Halley's comet / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Robert W. Farquhar, William H. Wooden, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Maintenance instructions direct support : launcher, rocket, armored vehicle mounted, M270, (1055-01-092-0596) : multiple launch rocket system. ([Washington, D.C.] : Dept. of the Army, 1984-), by United States. Department of the Army (page images at HathiTrust)
Maintenance instructions direct support launcher, rocket, armored vehicle mounted, M270 (1055-01-092-0596) : multiple launch rocket system. ([Washington, D.C.] : Dept. of the Army, 1984-), by United States. Department of the Army (page images at HathiTrust)
Maintenance instructions, general support launcher, rocket, armored vehicle mounted, M270, (1055-01-092-0596) : Multiple Launch Rocket System. ([Washington, D.C.] : Dept. of the Army, 1984-), by United States. Department of the Army (page images at HathiTrust)
Operator and organizational maintenance manual : 762-mm rockets MGR-1A and MGR-1B, (Honest John rocket system). ([Washington, D.C.] : Headquarters, Dept. of the Army, 1985-), by United States. Department of the Army (page images at HathiTrust)
Operator's manual : launcher, rocket, armored vehicle mounted, M270, (1055-01-092-0596), Multiple Launch Rocket System. ([Washington, D.C.] : Dept. of the Army, 1985-), by United States. Department of the Army (page images at HathiTrust)
Direct support and general support maintenance manual (including repair parts and special tools list) for 2.75-inch low spin, folding fin aircraft rockets, 66-mm light antitank weapon systems, 3.5-inch rockets and M3A2E1 rocket motor (JATO). ([Washington, DC] : Headquarters, Dept. of the Army, [1989-), by United States. Department of the Army (page images at HathiTrust)
Operator's manual for 66mm light antitank weapon system M72A1, M72A2 with coupler, M72A3 and practice rocket launcher M190 with M73 practice rocket. (Washington, DC : Dept. of the Army, [1989]), by United States. Department of the Army (page images at HathiTrust)
Equipment improvement report and maintenance digest : Multiple Launch Rocket System, first quarter, CY 1984. ([Washington, DC] : Headquarters, Dept. of the Army, 1984), by United States. Department of the Army (page images at HathiTrust)
Equipment improvement report and maintenance digest : Multiple Launch Rocket System, second quarter, CY 1984. ([Washington, D.C.] : Dept. of the Army, 1985-), by United States. Department of the Army (page images at HathiTrust)
Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant : II. Equilibrium composition / (Washington : National Advisory Committee for Aeronautics, [1956]), by Vearl N. Huff, Sanford Gordon, Anthony Fortini, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Prediction of explosive yield and other characteristics of liquid propellant rocket explosions : final report, October 13, 1968 / (Gainesville, Fla. : University of Florida, Florida Engineering and Industrial Experiment Station, Dept. of Mechanical Engineering, 1968), by Erich A. Farber, C. F. Bonzon, and F. W. Klement (page images at HathiTrust; US access only)
Static aerodynamic characteristics of a three-stage rocket vehicle having various fin configurations at low subsonic Mach numbers and angles of attack up to 28 ̊/ (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1963), by Clarence A. Brown, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
United States space launch strategy : hearing before the Subcommittee on Space and Aeronautics of the Committee on Science, U.S. House of Representatives, One Hundred Fourth Congress, second session, June 12, 1996. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1996), by United States. Congress. House. Committee on Science. Subcommittee on Space and Aeronautics (page images at HathiTrust)
Presenting the Pacific rocket society. ([South Pasadena, Calif., Pacific rocket soc., 1947?]), by Pacific Rocket Society (page images at HathiTrust)
Design and experimental performance of a small centrifugal pump for liquid hydrogen / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by George W. Lewis, Melvin J. Hartmann, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
Thermal decomposition and explosion of ammonium perchlorate and ammonium perchlorate propellant up to 50 kilobars (5.0 x 10⁹ N/m²) [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Hans R. Voelkl, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Effective thermal conductivities of four metal-ceramic composite coatings in hydrogen-oxygen rocket firings [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Ralph L. Schacht, Richard J. Quentmeyer, Harold G. Price, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
Cold-air performance evaluation of scale model oxidizer pump-drive turbine for the M-1 hydrogen-oxygen rocket engine. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Roy G. Stabe, John F. Kline, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental measurements of expanding storable-propellant products simulated by combustion of gaseous reactants / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Robert Friedman, Erwin A. Lezberg, Raymond E. Gaugler, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
FORTRAN IV computer program for calculation of thermodynamic and transport properties of complex chemical systems [electronic resource] / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : National Technical Information Service, 1973), by Roger A. Svehla, Bonnie J. McBride, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Allocation of single-stage-to-orbit research funds : hearing before the Subcommittee on Space of the Committee on Science, Space, and Technology, U.S. House of Representatives, One Hundred Third Congress, second session, July 19, 1994. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1994), by Space United States. Congress. House. Committee on Science (page images at HathiTrust)
U.S. commercial space launch competitiveness, parts 1 and 2 : hearings before the Subcommittee on Space and Aeronautics of the Committee on Science, House of Representatives, One Hundred Sixth Congress, first session, April 21 and June 10, 1999. (Washington : U.S. G.P.O. : For sale by the U.S. G.P.O., Supt. of Docs., Congressional Sales Office, 1999), by United States. Congress. House. Committee on Science. Subcommittee on Space and Aeronautics (page images at HathiTrust)
Computational study of single-expansion-ramp nozzles with external burning / ([Washington, D.C.] : National Aeronautics and Space Administration ; [Springfield, Va. : National Technical Information Service, distributor, 1994]), by Shaye Yungster, Charles J. Trefny, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Fin loads and tip-control hinge moments on a 1/8-scale model simulating the first stage of the Scout research vehicle at a mach number of 2.01 / (Washington [D.C.] : National Aeronautics and Space Administration, [1960]), by Ross B. Robinson, Emma Jean Landrum, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Diffusion algorithms and data reduction routine for onsite launch predictions for the transport of Titan III C exhaust effluents / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by J. Briscoe Stephens, P. A. Hamilton, and George C. Marshall Space Flight Center (page images at HathiTrust)
Ring-baffle pressure distribution and slosh damping in large cylindrical tanks / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Harland F. Scholl, Phillip K. Davis, David G. Stephens, and Langley Research Center (page images at HathiTrust)
Bivariate extreme value distributions / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by M. Elshamy, George C. Marshall Space Flight Center. Space Sciences Laboratory, and University of Alabama in Huntsville. Dept. of Mathematical Sciences (page images at HathiTrust)
Experimental evaluation of throat inserts in a storable-propellant rocket engine / (Washington, D.C. : National Aeronautical and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Jerry M. Winter, James R. Johnston, Larry D. Plews, and Lewis Research Center (page images at HathiTrust)
Rocket booster control : penalty functions and bounded phase coordinate control / (Washington, D.C. : NASA, [1964]), by D. L. Russell, Minneapolis-Honeywell Regulator Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Static longitudinal stability of a rocket vehicle having a rear-facing step ahead of the stabilizing fins / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Robert J. Keynton, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Free-flight investigation of the deployment, dynamic stability, and control characteristics of a 1/12-scale dynamic radio-controlled model of a large booster and parawing / (Washington [D.C.] : NASA, 1963), by Sanger M. Burk, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
An experimental evaluation of metallic diaphragms for positive fuel expulsion in the Atmosphere Explorer hydrazine propulsion subsystem / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by William L. Woodruff and Goddard Space Flight Center (page images at HathiTrust)
Analysis of axisymmetrical vibration of a partially liquid-filled elastic sphere by the method of Green's function / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Rudolf F. Glaser and George C. Marshall Space Flight Center (page images at HathiTrust)
An experimental investigation of two-phase liquid oxygen pumping / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Loren A. Gross and George C. Marshall Space Flight Center. Astronautics Laboratory (page images at HathiTrust)
Theoretical performance of hydrogen-oxygen rocket thrust chambers, (Washington, U.S. G.P.O., 1961), by Gilbert K. Sievers, George R. Kinney, and William A. Tomazic (page images at HathiTrust)
Flow in the base region of axisymmetric and two-dimensional configurations / (Washington, DC : U.S. G.P.O., 1961), by Milton A. Beheim, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
Comparative evaluation of test methods to simulate acoustic response of shroud-enclosed spacecraft structures / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by F. J. On and Goddard Space Flight Center (page images at HathiTrust)
Longitudinal oscillation of launch vehicles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Rudolf F. Glaser and George C. Marshall Space Flight Center (page images at HathiTrust)
Apollo experience report : launch escape propulsion subsystem / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Neil A. Townsend and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Apollo experience report : spacecraft heating environment and thermal protection for launch through the atmosphere of the earth / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Robert L. Dotts and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Analytic and experimental evaluation of shadow shields and their support members for thermal control of space vehicles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert J. Boyle, Robert J. Stochl, and Lewis Research Center (page images at HathiTrust)
Pressurant requirements for discharge of liquid methane from a 1.52-meter- (5-ft- ) diameter spherical tank under both static and slosh conditions / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Richard L. DeWitt, Thomas O. McIntire, and Lewis Research Center (page images at HathiTrust)
Launch, low-speed, and landing characteristics determined from the first flight of the North American X-15 research airplane / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Thomas W. Finch, Gene J. Matranga, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rocket booster control : time optimal control with amplitude and rate limited controls / (Washington, D.C. : NASA, 1964), by W. W. Schmaedeke, D. L. Russell, Minneapolis-Honeywell Regulator Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rocket booster control : Control of plants whose representation contains derivatives of the control variables / (Washington, D.C. : NASA, 1964), by W. W. Schmaedeke, Minneapolis-Honeywell Regulator Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rocket booster control : a sufficient condition in optimal control / (Washington, D.C. : NASA, 1964), by E. B. Lee, Minneapolis-Honeywell Regulator Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Research and development of propellant feed systems for ion engines / (Washington : National Aeronautics and Space Administration : Springfield, Va. : for sale by the National Technical Information Service, 1964), by Patrick J. Lawlor, United States National Aeronautics and Space Administration, and inc. New Products Research Thompson Ramo Wollbridge (page images at HathiTrust)
Electrothermal engine propellant storage and feed system study, phase II / (Washington : National Aeronautics and Space Administration : Springfield, Va. : for sale by the National Technical Information Service, 1964), by G. E. Roos, United States National Aeronautics and Space Administration, and Beach Aircraft Corporation (page images at HathiTrust)
Design and fabrication of an internally insulated filament wound liquid hydrogen propellant tank / ([Washington] : National Aeronautics and Space Administration, [1964]), by C. B. Shriver, Goodyear Aerospace Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Study to optimize gellant polymer-water systems for the control of hypergolic spills and fires / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by R. R. Jennings, Ames Research Center, and Dow Chemical USA. (page images at HathiTrust)
Technique for predicting high-frequency stability characteristics of gaseous-propellant combustors / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Richard J. Priem, Jefferson Y. S. Yang, and Lewis Research Center (page images at HathiTrust)
Lunar missions using chemical propulsion : system design issues / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Bryan A. Palaszewski and Lewis Research Center (page images at HathiTrust)
Theoretical investigation of the absorptive properties of small particles and heavy-atom gases / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by N. L. Krascella, United Aircraft Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A study of two phase detonation as it relates to rocket motor combustion instability / (Washington, DC : National Aeronautics and Space Administration ; Springfield, VA : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1965), by J. A. Nicholls, Kenneth W. Ragland, Eliahou K. Dabora, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Improved guidance hardware study for the Scout launch vehicle / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Roger T. Schappel, Langley Research Center, and Martin Marietta Corporation (page images at HathiTrust)
Computer programs for pressurization (ramp) and pressurized expulsion from a cryogenic liquid propellant tank / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Philip A. Masters and Lewis Research Center (page images at HathiTrust)
Centaur space vehicle pressurized propellant feed system tests. (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Lewis Research Center (page images at HathiTrust)
Theoretical investigation of the absorption and scattering of small particles / ([Washington] National Aeronautics and Space Administration, [1965]), by N. L. Krascella, United Aircraft Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Dynamic characteristics of a two-stage variable-mass flexible missile with internal flow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Leonard Meirovitch, John Bankovskis, Langley Research Center, and University of Cincinnati (page images at HathiTrust)
Axisymmetric oscillation of a partially liquid-filled cylindrical shell container having hemispherical bulkheads / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Rudolf F. Glaser and George C. Marshall Space Flight Center (page images at HathiTrust)
Low-gravity reorientation in a scale-model Centaur liquid-hydrogen tank / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Jack A. Salzman, Raymond F. Lacovic, William J. Masica, and Lewis Research Center (page images at HathiTrust)
Basic performance of a multilayer insulation system containing 20 to 160 layers / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Robert J. Stochl and Lewis Research Center (page images at HathiTrust)
Aspect determination in lunar shadow on Explorer 35 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Harold E. Taylor, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
The smoke-trail method for obtaining detailed measurements of the vertical wind profile for application to missile-dynamic-response problems / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Robert M. Henry, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Experimental investigation of liquid outflow from cylindrical tanks during weightlessness / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Joseph D. Derdul, Donald A. Petrash, Lynn S. Grubb, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Analytical determination of the effect of thermal property variations on the performance of a charring ablator / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by C. M. Pittman, William D. Brewer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A feasibility study on the use of wind profilers to support space shuttle launches / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Russell B. Chadwick, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Wave Propagation Laboratory (page images at HathiTrust)
A Guide to KSC. ([Greenbelt, Md.] : NASA GSFC Flight Projects Directorate, [1991]), by Goddard Space Flight Center. Flight Projects Directorate (page images at HathiTrust)
Space research : rocket launches and similar experiments at Cape Parry, Northwest Territories : understanding between the United States of America and Canada ... ([Washington] : U.S. Dept. of State : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1976), by etc. Canada United States. Treaties and United States Department of State (page images at HathiTrust)
Physical properties and thermodynamic functions of fuels, oxidizers, and products of combustion. (Santa Monica, Calif., Rand Corp., c1949-51), by Battelle Memorial Institute. Chemical Research Division (page images at HathiTrust; US access only)
Hall-effect magnetometers in scientific rocket payloads /, by Gordon M. Lerfald, Warner L. Ecklund, and Space Disturbances Laboratory (U.S.) (page images at HathiTrust)
Lightning hazard to rockets during launch I /, by Heinz W. Kasemir, Atmospheric Physics and Chemistry Laboratory (U.S.), and United States. Environmental Science Services Administration (page images at HathiTrust)
Lightning hazard to rockets during launch II /, by Heinz W. Kasemir, Atmospheric Physics and Chemistry Laboratory (U.S.), and United States. Environmental Science Services Administration (page images at HathiTrust)
The handling and storage of liquid propellants. (Washington, Office of the Director of Defense Research and Engineering, 1961), by United States. Advisory Panel on Fuels and Lubricants and United States. Office of the Director of Defense Research and Engineering (page images at HathiTrust)
Guided missiles and rockets, a bibliography, 1946-1956. (Fort Belvoir, Va., 1956), by Va.) Engineer School Library (Fort Belvoir (page images at HathiTrust)
Space cooperation : agreement between the United States of America and Australia, effected by exchange of notes, signed at Canberra September 1, 1987. (Washington, D.C. : Dept. of State : For sale by the Supt. of Docs., U.S. G.P.O., [1997?]), by Australia, etc. Australia United States. Treaties, and United States Department of State (page images at HathiTrust)
Rocket refractories. (China Lake, Calif. : U.S. Naval Ordnance Test Station, 1955), by Harry B. Porter, United States. Dept. of Commerce. Office of Technical Services, and Calif.). Propellants and Explosives Dept Naval Ordnance Test Station (Inyokern (page images at HathiTrust; US access only)
Results of the development motor 8 test firing : Hearing before the Subcommittee on Space Science and Applications of the Committee on Science, Space, and Technology, House of Representatives, One hundredth Congress, first session. September 16, 1987. (Washington : U.S. G.P.O. : For sale by the Supt. of Docs., Congressional Sales Office, U.S. G.P.O., 1987), by Space United States. Congress. House. Committee on Science (page images at HathiTrust)
Oceanographic and sea-floor surveys of underwater launch-sites : (5-16 May 1958) / (San Diego, Calif. : U.S. Navy Electronics Laboratory, [1959]), by Edwin C Buffington (page images at HathiTrust)
Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming equilibrium composition / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Sanford Gordon and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
Theoretical performance of JP-4 fuel and liquid oxygen as a rocket propellant : I. Frozen composition / (Washington : National Advisory Committee for Aeronautics, [1956]), by Vearl N. Huff, Anthony Fortini, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Theoretical performance of liquid ammonia with liquid oxygen as a rocket propellant / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Sanford Gordon and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
Theoretical performance of liquid hydrogen and liquid fluorine as a rocket propellant for a chamber pressure of 600 pounds per square inch absolute / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Anthony Fortine, Vearl N. Huff, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
Displacement and shattering of propellant droplets; final summary report (Washington, Air Force Office of Scientific Research, Combustion Dynamics Division, 1960), by E. Rabin, R. B. Lawhead, A. R. Schallenmuller, and Canoga Park Rocketdyne (page images at HathiTrust)
Principles of aircraft propulsion machinery. (New York, Pitman Pub. Corp., [1949]), by Israel Katz (page images at HathiTrust)
Range privatization : how fast, how soon, and how much? : hearing before the Subcommittee on Space and Aeronautics of the Committee on Science, House of Representatives, One Hundred Sixth Congress, second session, September 28, 2000. (Washington : U.S. G.P.O. : [U.S. G.P.O., Supt. of Docs., Congressional Sales Office, distributor], 2001), by United States. Congress. House. Committee on Science. Subcommittee on Space and Aeronautics (page images at HathiTrust)
Theoretical rocket performance of JP-4 fuel with mixtures of liquid ozone and fluorine / (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by Vearl N. Huff, Sanford Gordon, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
Rockets beyond the earth. (New York, McBride Co., [1954]), by Martin Caidin (page images at HathiTrust)
A compendium of aerobee sounding rocket launchings from 1959 through 1963 / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., 1966), by Jon R. Busse, Merril T. Leffler, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
Rocket science and missile engineering. (New York, Pen-Ink Pub. Co., [1959]), by Constantin Paul Lent (page images at HathiTrust)
Solid rocket thrust vector control. (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1974) (page images at HathiTrust)
Solid rocket motor nozzles / (Washington : NASA ; Springfield, Va. : For sale by the National Technical Information Service, 1975), by Russell A Ellis (page images at HathiTrust)
Liquid rocket engine nozzles / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Jack C. Hyde, G. S. Gill, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Magnetic plasma propulsion by means of a travelling sinusoidal field. (Los Angeles, Physical Research Laboratory, space Technology Laboratories, 1960), by Rudolf X. Meyer (page images at HathiTrust)
20th meeting bulletin. (Silver Spring, Md., Solid Propellant Information Agency, Applied Physics Laboratory, Johns Hopkins University; [reproduced by Armed Services Technical Information Agency, Arlington, Va., 1961?), by Riverside Joint Army-Navy-Air Force-ARPA-NASA Panel on Physical Properties of Solid Propellants. 20th meeting (page images at HathiTrust)
Interim report on the thermodynamics of chemical species important to rocket technology.. ([Washington], 1970), by United States. National Bureau of Standards (page images at HathiTrust)
Technology of missile science. ([Los Angeles?] : Produced by Air Science Associates of Southern California for the U. S. Air Force, Institute of Technology, Wright-Patterson Air Force Base, 1961), by James C. Propulsion systems Nielsen, J. F. Detwiler, and John Milton Lenoir (page images at HathiTrust)
Rockets, jets, and the atom. (New York, Pen-Ink Pub. Co., [1953, 1952]), by Constantin Paul Lent (page images at HathiTrust)
Structural design of missiles and spacecraft (New York, McGraw-Hill, 1962), by Lewis H Abraham (page images at HathiTrust)
Antiproton annihilation propulsion / (Edwards Air Force Base, Calif. : Air Force Rocket Propulsion Laboratory, Air Force Space Technology Center, Space Division, Air Force Systems Command, [1985]), by Robert L Forward, Forward Unlimited, University of Dayton. Research Institute, and Air Force Rocket Propulsion Laboratory (U.S.) (page images at HathiTrust)
Internal ballistics of solid-fuel rockets; miliary rockets using dry-processed double-base propellant as fuel. (New York, McGraw-Hill, 1950), by R. N. Wimpress (page images at HathiTrust)
Rockets, new trail to empire, review & bibliography ([Glen Ellyn, Ill., c1945]), by Robert Lee Farnsworth (page images at HathiTrust)
Jane's all the world's aircraft (New York : McGraw-Hill,), by Fred T. Jane (page images at HathiTrust)
Final environmental assessment for a launch operator license for Sea Launch Limited Partnership / ([U.S. : ICF Consulting, 2001]), by ICF Consulting Associates and United States. Office of Commercial Space Transportation (page images at HathiTrust; US access only)
NRL participation in the CSAGI rocket and satellite conference, September 30-October 5, 1957. (Washington, Distributed by OTS, U.S. Dept. of Commerce, 1959), by Naval Research Laboratory (U.S.) and International Council of Scientific Unions. Special Committee for the International Geophysical Year (page images at HathiTrust; US access only)
An investigation of the optimum design and flight of rockets / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by John D. Bird, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Measured performance of water vapor jets for space vehicle attitude control systems / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Gerd Kanning and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Dynamic performance analysis of a fuel-control valve for use in airbreathing engine research / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Peter G. Batterton, John R. Zeller, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Nerva control drum actuator irradiation test program / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by David J. Robinson, Richard R. Wyer, John T. Mayer, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Calculation of transport properties of ionizing atomic hydrogen / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1966), by Norman T. Grier, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust; US access only)
A design study of a regeneratively cooled nozzle for a Tungsten water-moderated nuclear rocket system / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Richard L. Puthoff, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Estimates of attenuation and reflection of telemetering signals by ionized flow fields surrounding typical reentry bodies / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Anthony J. Russo, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Comparison of rocket performance using exhaust diffuser and conventional techniques for altitude simulation / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Joseph N. Sivo, Daniel J. Peters, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Guided missiles, rockets and artificial satellites, including project vanguard ; a selected list of titles. ([Washington], 1957), by Army Library (U.S.) (page images at HathiTrust; US access only)
Airbreathing propulsion system testing using sweep frequency techniques / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Daniel I. Drain, Francis J. Paulovich, William M. Bruton, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Correlation of local heat-transfer coefficients for single-phase turbulent flow of hydrogen in tubes with temperature ratios to 23 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Maynard F. Taylor and Lewis Research Center (page images at HathiTrust)
From a scientific heritage, ([Washington] National Aeronautics and Space Administration, for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va., [1969]), by F. A. T︠S︡ander (page images at HathiTrust; US access only)
Analytical method for steady state heat transfer in two-dimensional porous media / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Robert Siegel, Marvin E. Goldstein, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Experimental investigation of close-range rocket-exhaust impingement on surfaces in a vacuum / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Leonard V. Clark, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Dimple, spall and perforation characteristics of thin plates of nine materials under hypervelocity impact / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and technical Information, Springfield, Va. 22151], 1970), by Nestor Clough, Allen R. McMillan, Seymour Lieblein, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Comparison of small water-graphite nuclear rocket stages with chemical upper stages for unmanned missions / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by M. Ray Clark, Gerald P. Lahti, Gary D. Sagerman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
IMP I optical aspect system / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by E. J. Pyle, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Baffle thickness effects in fuel sloshing experiments / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Henry A. Cole and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Vibration analysis of clustered launch vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1965), by Rudolf F. Glaser, Everette E. Beam, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Amplification by wave distortion of the dynamic response of vaporization limited combustion / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Marcus F. Heidmann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Axial and circumferential variations of hot-gas-side heat-transfer rates in a hydrogen-oxygen rocket / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Ralph L. Schacht, Richard J. Quentmeyer, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Freezing rain experiments, Project Freeze; final report. Contract no. Nonr-2250(00) (Buffalo, Cornell Aeronautical Laboratory, Inc., 1961), by Harold F. Meese (page images at HathiTrust)
Space launch vehicles. Hearings, Eighty-ninth Congress, first session, on national space launch vehicles. January 26-27, 1965. (Washington, U. S. Govt. Print. Off., 1965), by United States. Congress. Senate. Committee on Aeronautical and Space Sciences (page images at HathiTrust)
Handling and use of fluorine and fluorine-oxygen mixtures in rocket systems, (Washington : Scientific and Technical Information Division, Office of Technology Utilization, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1967), by Harold W. Schmidt (page images at HathiTrust)
Perfect bell nozzle parametric and optimization curves / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by J. L. Tuttle, D. H. Blount, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Technical Symposium, Materials Research, Development, and Application, 9-10 July 1958, Statler-Hilton Hotel, Dallas, Texas. [Technical papers. (Washington, 1958]), by United States. Air Force. Air Research and Development Command. cn and Materials Research Technical Symposium (page images at HathiTrust)
Solid propellant rockets, an introductory handbook. (Wyandotte, Mich., American Rocket Co., 1955 [i.e. 1956]), by Alfred J. Zaehringer (page images at HathiTrust)
Effect of temperature and gap opening rate on the resiliency of candidate solid rocket booster O-ring materials / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Cynthia L. Lach and Langley Research Center (page images at HathiTrust)
Liquid hydrogen as a propulsion fuel, 1945-1959 / (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration, 1978), by John L. Sloop (page images at HathiTrust)
Computer program for calculation of complex chemical equilibrium compositions, rocket performance, incident and reflected shocks, and Chapman-Jouguet detonations / (Washington, D.C. : Scientific and Technical Information Office, National Aeronautics and Space Administration, 1976 i.e. 1980), by Sanford Gordon, Bonnie J. McBride, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Defense acquisition : examination of MLRS Terminal Guidance Warhead program : report to congressional committees / (Washington, DC : The Office, 1991), by United States General Accounting Office (page images at HathiTrust)
Aerospace testing : promise of closer NASA/DOD cooperation remains largely unfulfilled : report to the Chairman and Ranking Minority Member, Subcommittee on Science, Technology and Space, Committee on Commerce, Science and Transportation, U.S. Senate / (Washington, D.C. (P.O. Box 37050, Washington, D.C. 20013) : The Office, [1998]), by United States General Accounting Office and Science United States. Congress. Senate. Committee on Commerce (page images at HathiTrust)
Rockets : a teacher's guide with activities in science, mathematics, and technology. (Washington, DC : National Aeronautics and Space Administration, Office of Human Resources and Education, Education Division ; Houston, Tex. : Education Working Group, NASA Johnson Space Center, [1999]), by Lyndon B. Johnson Space Center. Education Working Group and United States. National Aeronautics and Space Administration. Education Division (page images at HathiTrust)
The dynamic behavior of liquids in moving containers, with applications to space vehicle technology. (Washington, Scientific and Technical Information Division, National Aeronautics and Space Administration; for sale by Supt. of Docs., U. S. Govt. Print. Off., 1966 [i.e. 1967]), by H. Norman Abramson and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rockets : an educator's guide with activities in science, mathematics, and technology. (Washington, DC : National Aeronautics and Space Administration, Office of Human Resources and Education, Office of Education ; Houston, TX : Teaching From Space Program, NASA Johnson Space Center, [2003]), by Teaching from Space Program (Lyndon B. Johnson Space Center) and United States. National Aeronautics and Space Administration. Office of Education (page images at HathiTrust)
A computational model for the prediction of jet entrainment in the vicinity of nozzle boattails (The BOAT code) / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Service ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Sanford M. Dash, Harold S. Pergament, Aeronautical Research Associates of Princeton, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Low-density foam for insulating liquid-hydrogen tanks / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Irving E. Sumner, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
Management of cryogenic propellants in a full-scale orbiting space vehicle / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Raymond F. Lacovic, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rockets, information and activities for elementary teachers to use in preparing students for a unit on model rocketry / ([Washington, D.C.?] : National Aeronautics and Space Administration, [1992]), by Gregory Vogt and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental thrust performance of a high-area-ratio rocket nozzle / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Albert J. Pavli, Tamara A. Smith, Kenneth J. Kacynski, and Lewis Research Center (page images at HathiTrust)
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m² (350 psia) / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Tamara A. Smith, Albert J. Pavli, Lewis Research Center, and Kenneth J. Kacynski (page images at HathiTrust)
Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Kenneth J. Kacynski, Tamara A. Smith, Albert J. Pavli, and Lewis Research Center (page images at HathiTrust)
Analysis of quasi-hybrid solid rocket booster concepts for advanced earth-to-orbit vehicles / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Robert L. Zurawski, Douglas C. Rapp, and Lewis Research Center (page images at HathiTrust)
Compatibility of dispersion-strengthened platinum with resistojet propellants / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1987), by Margaret V. Whalen, Michael V. Nathal, and Lewis Research Center (page images at HathiTrust)
Rocket flight engineering / ([Washington] : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Eugen Sänger (page images at HathiTrust)
A method of dynamic programming and its application to optimization problems of flight mechanics / ([Washington, D.C. :] National Aeronautics and Space Administration, [1967]), by Werner Schulz and H.-K. Schulze (page images at HathiTrust)
A new method of approaching the design of sounding rockets / (Washington : National Aeronautics and Space Administration, 1967), by Ernesto Gismondi and Convegno Internazionale delle Communicazioni (13th : 1965 : Genoa) (page images at HathiTrust)
Launch vehicle effluent measurements during the May 12, 1977, Titan III launch at Air Force Eastern Test Range / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Gerald L. Gregory, David C. Woods, Richard J. Bendura, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Launch vehicle effluent measurements during the August 20, 1977, Titan III launch at Air Force Eastern Test Range / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by David C. Woods, Dewey E. Wornom, Richard J. Bendura, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Experimental evaluation of several ablative materials as nozzle sections of a storable-propellant rocket engine / (Washington, D.C. : National Aeronautical and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1966), by Donald A. Peterson, Carl L. Meyer, and Lewis Research Center (page images at HathiTrust)
Effluent monitoring of the December 10, 1974, Titian III-E launch at Air Force Eastern Test Range, Florida / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by Dewey E. Wornom, David C. Woods, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Space processing application rocket project : SPAR V final report. (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by D. Schaefer, F. Reeves, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
Experimental measurements of the ground cloud effluents and cloud growth for the May 20, 1975, Titan IIIC launch at Air Force Eastern test Range, Florida / ([Washington] : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Information Service, 1977), by Gerald L. Gregory, Richard W. Storey, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rapid estimation of concentration of aromatic classes in middistillate fuels by high-performance liquid chromatography / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Dumas A. Otterson, Gary T. Seng, and Lewis Research Center (page images at HathiTrust)
Thermodynamic analysis of an axial-flow laser-powered thruster / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Albert F. Kascak and Lewis Research Center (page images at HathiTrust)
Wind-weighting for sounding rockets with a telemetry system / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by Frank M. Boykin and Wallops Flight Facility (page images at HathiTrust)
Performance capability of laser-powered launch vehicles using vertical ascent trajectories / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Omer F. Spurlock and Lewis Research Center (page images at HathiTrust)
Upper stages using liquid propulsion and metallized propellants / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Bryan A. Palaszewski and Lewis Research Center (page images at HathiTrust)
Abort separation study of a shuttle orbiter and external tank at hypersonic speeds / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Peter T. Bernot and Langley Research Center (page images at HathiTrust)
Space processing applications rocket project : SPAR final report / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by George C. Marshall Space Flight Center and United States National Aeronautics and Space Administration (page images at HathiTrust)
Apollo Saturn 511 effluent measurements from the Apollo 16 launch operations : an experiment / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Gerald L. Gregory, Dewey E. Wornom, William C. Hulten, and Langley Research Center (page images at HathiTrust)
Experimental evaluation of a pilot multinozzle-duct apparatus / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Richard L. Puster, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
Single launch lunar habitat derived from NSTS external tank / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Charles B. King and Langley Research Center (page images at HathiTrust)
Space processing applications rocket project : SPAR VI final report / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by R. Chassay, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Surface recession characteristics of a cryogenic insulation subjected to arc-tunnel heating / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by C. M. Pittman, Ronald D. Brown, and Langley Research Center (page images at HathiTrust)
Space Processing Applications Rocket (SPAR) Project : SPAR IX final report / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1984), by Richard M. Poorman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Some effects of thermal-cycle-induced deformation in rocket thrust chambers / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by Ned P. Hannum, Harold G. Price, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
Modeling of space vehicle propellant mixing / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by John C. Aydelott and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
Doctor Langley's paradox: two letters suggesting the development of rockets. (Washington, Smithsonian Institution, 1960), by Russell J Parkinson (page images at HathiTrust)
Rapid optimization of multiple-burn rocket flights / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1969), by K. R. Brown, G. W. Johnson, E. F. Harrold, George C. Marshall Space Flight Center, and International Business Machines Corporation. Federal Systems Division (page images at HathiTrust)
Capacitance discharge system for ignition of Single Bridge Apollo Standard Initiators (SBASI) / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by R. D. Ward, Langley Research Center, and LTV Aerospace Corporation. Vought Systems Division (page images at HathiTrust)
Analysis and test for space shuttle propellant dynamics / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Robert L. Berry, Leonard J. Demchak, James R. Tegart, Lyndon B. Johnson Space Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Martin Marietta Denver Aerospace (page images at HathiTrust)
Performance investigation of a nonpumping rocket-ejector system for altitude simulation / (Washington : National Aeronautics and Space Administration, [1959]), by Anthony Fortini and Lewis Research Center (page images at HathiTrust)
Aerodynamic-heating data obtained from free-flight tests between Mach numbers of 1 and 5 / (Washington : National Aeronautics and Space Administration, [1960]), by Charles B. Rumsey, Russell N. Hopko, Robert Owens Piland, and Langley Research Center (page images at HathiTrust)
Flight report, Interplanetary Monitoring Platform IMP-II (Explorer XXI) / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Frank A. Carr and Goddard Space Flight Center (page images at HathiTrust)
Experimental study of zero-flow ejectors using gaseous nitrogen / (Washington : National Aeronautics and Space Administration, [1960]), by William Leroy Hill Jones, Carl F. Lorenzo, Harold G. Price, and Lewis Research Center (page images at HathiTrust)
Measurement of liquid and two-phase hydrogen densities with a capacitance density meter / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by George E. Turney, Roger W. Snyder, and Lewis Research Center (page images at HathiTrust)
A simulation investigation of the loads experienced by a piloted launch vehicle / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Robert K. Sleeper and Langley Research Center (page images at HathiTrust)
Velocity modification for earth capture of an astronomical body in the solar system / (Washington : National Aeronautics and Space Administration, [1961]), by Su-Shu Huang (page images at HathiTrust)
Equipment and procedures for glass-bead peening titanium-alloy tanks / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Thomas T. Bales, W. Barry Lisagor, Charles R. Manning, and Langley Research Center (page images at HathiTrust)
Stress-corrosion cracking of Ti-6Al-4V titanium alloy in nitrogen tetroxide / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by W. Barry Lisagor, Thomas T. Bales, Charles R. Manning, and Langley Research Center (page images at HathiTrust)
Experimental study of aeroelastic instability of overexpanded rocket nozzle extensions / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by W. J. Tuovila, Norman S. Land, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Estimates of local and average fuel temperatures in a gaseous nuclear rocket engine / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Albert F. Kascak and Lewis Research Center (page images at HathiTrust)
Experimental performance of a hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by William L. Jones, John W. Gibb, Carl A. Aukerman, and Lewis Research Center (page images at HathiTrust)
Materials / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by William D. Klopp and Lewis Research Center (page images at HathiTrust)
Investigation of injectors for a low-chamber-pressure hydrogen-fluorine rocket engine / (Washington, D.C. : National Aeronautics and Space Administration, 1962), by Harold G. Price, Arthur M. Shinn, Robert J. Lubick, and Lewis Research Center (page images at HathiTrust)
Elements of computers / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Robert L. Miller and Lewis Research Center (page images at HathiTrust)
Description of Langley low-frequency noise facility and study of human response to noise frequencies below 50 cps / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Philip M. Edge, William H. Mayes, and Langley Research Center (page images at HathiTrust)
Monthly and annual wind distribution as a function of altitude for Patrick Air Force Base, Cape Canaveral, Florida / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by J. W. Smith, William W. Vaughan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Description and performance of three Trailblazer II reentry research vehicles / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Reginald R. Lundstrom, W. Ray Hook, Allen B. Henning, and Langley Research Center (page images at HathiTrust)
A technique for predicting far-field acoustic environments due to a moving rocket sound source / (Washington : National Aeronautics and Space Administration, [1963]), by G. A. Wilhold, J. H. Jones, S. H. Guest, and George C. Marshall Space Flight Center. Propulsion and Vehicle Engineering Division (page images at HathiTrust)
Minimum fuel ascent from the lunar surface / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Albert E. Brown and Langley Research Center (page images at HathiTrust)
Aerodynamic stability characteristics of the Apollo launch escape vehicle (LEV) with canard surfaces deployed / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by William C. Moseley, Bass Redd, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
Effect of canards in reducing launch vehicle flight loads / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Everett C. Alexis, Raymond A. Turk, Kenneth I. Davidson, Robert W. Cubbison, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Fatigue of liquid rocket engine metals at cryogenic temperatures to -452 ̊F (4 ̊K) / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Alfred J. Nachtigall, John C. Freche, Stanley J. Klima, and Lewis Research Center (page images at HathiTrust)
Re-entry glide maneuvers for recovery of a winged first-stage rocket booster : Alan D. Levin and Edward J. Hopkins. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Alan D. Levin, Edward J. Hopkins, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Supersonic investigation of nozzle hinge moments of a modified Saturn C-1 model with and without jet flow / (Washington, D.C. : National Aeronautics and Space Administration, [1963]), by Nickolai Charczenko, Jerry L. Lowery, and Langley Research Center (page images at HathiTrust)
Performance charts for multistage rocket boosters / (Washington : National Aeronautics and Space Administration, [1961]), by John S. MacKay, Richard J. Weber, and Lewis Research Center (page images at HathiTrust)
Launch environment profiles for sounding rockets and spacecraft / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by William J. Neff, R. A. Montes de Oca, United States National Aeronautics and Space Administration, and Allen Applied Research Inc Booz (page images at HathiTrust)
Static aerodynamic characteristics of three rocket-vehicle configurations at Mach numbers from 1.80 to 4.63 including some effects of fin size, fin cant, and auxiliary rocket motors / (Washington : National Aeronautics and Space Administration, [1963]), by Dennis E. Fuller, Gerald V. Foster, and Langley Research Center (page images at HathiTrust)
Control of a large launch vehicle with limited thrust vectoring in the presence of winds / (Washington : National Aeronautics and Space Administration, [1963]), by Dennis F. Collins, Homer G. Morgan, and Langley Research Center (page images at HathiTrust)
Preliminary investigation of off-design performance of divergent-ejector-type rocket nozzles / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Laurence W. Gertsma, Richard A. Yeager, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Performance of a variable divergent-shroud ejector nozzle designed for flight mach numbers up to 3.0 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Andrew J. Stofan, James R. Mihaloew, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Experimental performance of liquid hydrogen and liquid fluorine in regeneratively cooled rocket engines / (Washington D.C. : National Aeronautics and Space Administration, 1959), by H. W. Douglass, H. G. Price, G. Hennings, and Langley Research Center (page images at HathiTrust)
Effects of canted forward faces on the static longitudinal stability characteristics of the escape and exit configurations of a project mercury capsule model at a mach number of 2.01 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Roy V. Harris, Ross B. Robinson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Heat transfer and boundary layer in conical nozzles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Donald R. Boldman, Robert W. Graham, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Ground cloud effluent measurements during the May 30, 1974, Titan III launch at the Air Force Eastern Test Range / (Washington : National Aeronautics and Space Administration ;, 1977), by Richard J. Bendura and Kenneth H. Crumbly (page images at HathiTrust)
Space shuttle pogo active controller design using frequency domain optimization / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Robert C. Seidel, Bruce Lehtinen, Carl F. Lorenzo, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
Theoretical investigation of radiant heat transfer in the fuel region of a gaseous nuclear rocket engine / ([Washington, D.C.] : National Aeronautics and Space Administration, [1967]), by A. S. Kesten and N. L. Krascella (page images at HathiTrust)
An experimental investigation of the viscous damping of liquid sloshing in spherical tanks / (Washington, D.C. : National Aeronautics and Space Administration, [1963]), by Irving E. Sumner, Andrew J. Stofan, and Lewis Research Center (page images at HathiTrust)
Relativistic rocket mechanics / (Washington : National Aeronautics and Space Administration, 1960), by Helmut G. L. Krause (page images at HathiTrust)
Recommendations and evaluations of materials-research areas of importance to missile and space vehicle structures / (Washington, D.C. : National Aeronautics and Space Administration, [1963]), by Jack B. Esgar, William Raymond Micks, Norris F. Dow, and United States. National Aeronautics and Space Administration. Research Advisory Committee on Missile and Space Vehicle Structures (page images at HathiTrust)
Longitudinal vibration characteristics of 1/10-scale Apollo/Saturn V replica model / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Larry D. Pinson, H. Wayne Leonard, and Langley Research Center (page images at HathiTrust)
Investigation of two-phase hydrogen flow in pump inlet line / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969), by Donald C. Urasek, Robert E. Connelly, Phillip R. Meng, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A thermocouple technique for measuring hot-gas-side wall temperatures in rocket engines / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Ronald G. Huff, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Variation of convective heat-transfer coefficient around a simulated rocket cooling tube section / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Ronald G. Huff, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Transonic wind-tunnel investigation of the fin loads of a 1/8-scale model simulating the first stage of the Scout research vehicle / (Washington : National Aeronautics and Space Administration, [1961]), by Thomas C. Kelly and Langley Research Center (page images at HathiTrust)
Effects of jet pluming on the static stability of five rocket models at Mach numbers of 4, 5, and 6 and static pressure ratios up to 26 000 / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by William F. Hinson, Robert J. McGhee, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Analysis of heat transfer in a bounded two-dimensional porous region and application to a porous square duct / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Marvin E. Goldstein, Robert Siegel, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A rapid method for optimization of the rocket propulsion system for single-stage-to-orbit vehicles / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Charles H. Eldred, Sabina V. Gordon, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Involute strip development method for fabrication of rotationally symmetrical double curved surfaces of revolution / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Rene E. Chambellan, Eugene J. Pleban, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Investigation of engine-exhaust-airframe interference on a cruise vehicle at Mach 6 / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by James M. Cubbage, F. S. Kirkham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Head to base transfer function characteristics of a cylindrical tank partly filled with liquid / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Carl F. Lorenzo, Eva T. Jun, William G. Costakis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Lateral vibration characteristics of the 1/10-scale Apollo/Saturn V replica model / (Washington, DC : National Aeronautics and Space Administration, 1970), by Ellwood L. Peele, Sumner A. Leadbetter, H. Wayne Leonard, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Design, fabrication, and structural testing of a lightweight shadow shield for deep-space application / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by David Miao, Richard L. DeWitt, James R. Barber, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Performance of an isolated two-dimensional wedge nozzle with fixed cowl and variable wedge centerbody at mach numbers up to 2.01 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Donald L. Maiden, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Comparison of prediction methods and studies of relaxation in hypersonic turbulent nozzle-wall boundary layers / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va. 22151], 1969), by Dennis M. Bushnell, William V. Feller, William D. Harvey, Charles B. Johnson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
A study of display systems for manual guidance of large launch vehicles utilizing the X-15 airplane and flight simulators / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Armando E. Lopez, Ronald M. Gerdes, Gordon H. Hardy, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
Longitudinal mass-spring modeling of launch vehicles / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Rudolf F. Glaser, United States National Aeronautics and Space Administration, and George C. Marshall Space Flight Center (page images at HathiTrust)
Some factors affecting the stress-corrosion cracking of Ti-6Al-4V alloy in methanol / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by W. Barry Lisagor, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
Method for calculating rocket engine structural loads / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Jerrell M. Thomas, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Vibration and stability analysis of compressed rocket vehicles / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1965]), by Rudolf F. Glaser and George C. Marshall Space Flight Center (page images at HathiTrust)
Hypervelocity impacts into stainless-steel tubes armored with reinforced beryllium / ([Washington, D.C.] : National Aeronautics and Space Administration ; Springfield, Va. : [National Technical Information Service, 1966]), by A. R. McMillan, James H. Diedrich, Nestor Clough, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Principles of design of dynamically similar models for large propellant tanks / (Washington : National Aeronautics and Space Administration, [1960]), by Paul E. Sandorff and Massachusetts Institute of Technology (page images at HathiTrust)
Operational experiences and characteristics of the X-15 flight control system / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert A. Tremant and United States National Aeronautics and Space Administration (page images at HathiTrust)
Asymmetric "Penshape" nozzles in jet-canard configurations for attitude control / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Robert W. Cubbison and United States National Aeronautics and Space Administration (page images at HathiTrust)
Combustion instability limits determined by a nonlinear theory and a one-dimensional model / by Richard J. Priem and Donald C. Guentert. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], 1962), by Richard J. Priem, Donald C. Guentert, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Evaluation of a pilot describing function method applied to the manual control analysis of a large flexible booster / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Dallas G. Denery, Brent Y. Creer, and Ames Research Center (page images at HathiTrust)
Experimental bending strength of an Atlas LV-3C booster beyond compressive skin wrinkling / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Robert P. Miller and Lewis Research Center (page images at HathiTrust)
Investigation of the aerodynamic characteristics of two preliminary designs of Scout research vehicle at Mach numbers from 1.77 to 4.65 / (Washington : National Aeronautics and Space Administration, [1961]), by Robert J. Keynton, Ann B. Fichter, and Langley Research Center (page images at HathiTrust)
Measurement techniques investigated for detection of hydrogen chloride gas in ambient air / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Gerald L. Gregory, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
Rocket research; history and handbook. (New York, Pen-ink pub. co., [c1945]), by Constantin Paul Lent (page images at HathiTrust)
Selected welding techniques, from George C. Marshall Space Flight Center, Manufacturing Engineering Division, Huntsville, Alabama. (Washington] National Aeronautics and Space Administration; [for sale by the superintendent of Documents, U. S. Govt. Print. Off., 1964]), by United States. National Aeronautics and Space Administration. Technology Utilization Division (page images at HathiTrust)
Jet aircraft simplified. (Los Angeles, Aero Publishers, 1950), by Charles Edward Chapel (page images at HathiTrust)
A wind-compensation method and results of its application to flight tests of twelve trailblazer rocket vehicles / (Washington, D.C. : National Aeronautics and Space Administration, 1964), by Allen B. Henning, Jean C. Keating, Reginald R. Lundstrom, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
1000-hour endurance test of a glass-coated accelerator grid on a 15-centimeter-diameter Kaufman thruster / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Bruce A. Banks, Robert T. Bechtel, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
An analytical method for determining the multi-layer thickness and regression rates for a hybrid or tribrid rocket motor / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by Walter Brooks Drew, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Solar absorptances and spectral reflectances of 12 metals for temperatures ranging from 300 to 500 K / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Ernie W. Spisz, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Tensile and cyclic fatigue properties of graphite filament-wound pressure vessels at ambient and cryogenic temperatures / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Morgan P. Hanson, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Effects of wall pressure distribution and liquid temperature on incipient cavitation of freon-114 and water in venturi flow / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1968), by Royce D. Moore, Thomas F. Gelder, Robert S. Ruggeri, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Nonequilibrium calculations of methane-fluorine-oxygen and butene-1-fluorine-oxygen rocket performance / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by David A. Bittker, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Missiles, rockets and satellites. (Washington, 1958) (page images at HathiTrust; US access only)
Range privatization : how fast, how soon, and how much? : hearing before the Subcommittee on Space and Aeronautics of the Committee on Science, House of Representatives, One Hundred Sixth Congress, second session, September 28, 2000. (Washington : U.S. G.P.O. : [U.S. G.P.O., Supt. of Docs., Congressional Sales Office, distributor], 2001), by United States. Congress. House. Committee on Science. Subcommittee on Space and Aeronautics (page images at HathiTrust)
Guided missiles in foreign countries, prepared for the Committee on Armed Services, United States Senate, Eighty-fifth Congress, first session, (Washington : U. S. Govt. Print. Off., 1957), by Library of Congress Legislative Reference Service, Eilene Marie Slack Galloway, and United States Senate Committee on Armed Services (page images at HathiTrust)
General procurement information on guided missile programs, rockets and target drones. (Washington, D.C. : Office of the Secretary of Defense, Central Military Procurement Information Office, 1959), by United States. Central Military Procurement Information Office (page images at HathiTrust; US access only)
Performance and stability characteristics of nitrogen tetroxide : hydrazine combustors / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Martin Hersch and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Analytical and experimental investigation of outflow residuals in interconnected spherical tanks / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Harold J. Kasper, Robert J. Boyle, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Rockets, missiles, and satellites. (New York, Grosset & Dunlap, [1958]), by Clayton Knight (page images at HathiTrust; US access only)
Fundamentals of rocket propulsion / (New York : Reinhold, [1960]), by Raymond E. Wiech and Robert F. Strauss (page images at HathiTrust)
Annotated bibliography of space science and technology with an astronomical supplement. A history of astronautical book literature--1931 through 1961. (Washington, Arfor Publications, [1962]), by Frederick I. Ordway (page images at HathiTrust)
Rockets and guided missiles; (New York, Macmillan Co., [1956]), by John Humphries (page images at HathiTrust)
Modern flight dynamics. (Englewood Cliffs, N.J., Prentice-Hall, 1961), by W. Richard Kolk (page images at HathiTrust)
Supersonic aerodynamics and rocket propulsion, (Los Angeles, c1963]), by Robert F. Lee (page images at HathiTrust)
Jets, rockets, and guided missiles, (New York, McBride, [1951]), by David C. Cooke (page images at HathiTrust)
Jet propulsion, (Elizabeth, N.J., 1944), by Thomas N. Dalton (page images at HathiTrust; US access only)
Rocketry and jet-propulsion. (New York, Pen-Ink Pub. Co., [1951]), by Constantin Paul Lent (page images at HathiTrust)
Rocket development ; liquid-fuel rocket research, 1929-1941. (New York : Prentice-Hall, 1948), by Robert Hutchings Goddard, G. Edward Pendray, and Esther Christine Kisk Goddard (page images at HathiTrust)
Rocketry and space exploration. (Princeton, N.J., Van Nostrand, [1958]), by Andrew G. Haley (page images at HathiTrust)
Theoretical evaluation of chemical propellants. (Englewood Cliffs, N. J., Prentice-Hall, [1963]), by Roger Lawrence Wilkins (page images at HathiTrust)
The handbook of rockets and guided missiles. (Chicago, Perastadion Press, 1957), by Norman J. Bowman (page images at HathiTrust)
J-P fundamentals ... (Elizabeth, N. J., c1944), by Thomas N. Dalton (page images at HathiTrust)
USSR missile and rocket program: bibliography. ([Washington], 1961), by Library of Congress. Aerospace Technology Division (page images at HathiTrust)
The handling and storage of liquid propellants. (Washington, Office of the Director of Defense Research and Engineering, 1963), by United States. Advisory Panel on Fuels and Lubricants and United States. Office of the Director of Defense Research and Engineering (page images at HathiTrust)
Turbine- and jet-propelled aircraft powerplants. (New York, Chartwell House, 1954), by James P. Eames (page images at HathiTrust)
Bibliography of books and published reports on gas turbines, jet propulsion and rocket power plants January 1950 through December 1953. (Washington, U.S. Govt. Print. Off., 1954), by Ernest Franklin Fiock and Carl Halpern (page images at HathiTrust)
Environmental safety aspects of nuclear rocket flight operations : quarterly progress report : for Space Nuclear Propulsion Office, Atomic Energy Commission, National Aeronautics and Space Administration., by sponsor U.S. Atomic Energy Commission and sponsor United States. Space Nuclear Propulsion Office (page images at HathiTrust)
Particle reentry interactions /, by Ralph S. Decker, Morton I. Goldman, sponsor U.S. Atomic Energy Commission, and sponsor United States. Space Nuclear Propulsion Office (page images at HathiTrust)
The use of acoustic scale models for investigating near field noise of jet and rocket engines / (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, U. S. Air Force, 1961), by Walter V. Morgan, Kenneth J. Young, L. C. Sutherland, and Boeing Company. Aero-Space Division (page images at HathiTrust)
Jane's all the world's aircraft. (London [etc.] : Jane's Information Group [etc.], 1909-), by Fred T. Jane and Jane's Information Group (page images at HathiTrust; US access only)
Survey of Japanese space program with emphasis on Kappa and Lambda type observation rockets, ([Washington] National Aeronautics and Space Administration; for sale by the Office of Technical Services, Dept. of Commerce, [1965]), by Hideo Itokawa (page images at HathiTrust; US access only)
Exploratory rocket flight tests to investigate the use of a freely spinning monoplane tail for stabilizing a body / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Paul E. Purser, Joseph E. Stevens, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Theoretical performance of JP-4 fuel with a 70-percent-fluorine - 30-percent oxygen as a rocket propellant. (Washington, D.C. : National Advisory Committee for Aeronautics, 1956), by Sanford Gordon, Vearl N. Huff, Lewis Flight Propulsion Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
A method for determining turbine design characteristics for rocket turbodrive applications / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Warner L. Stewart, Warren J. Whitney, David G. Evans, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Summary of flutter experiences as a guide to the preliminary design of lifting surfaces on missiles / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Dennis J. Martin, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Investigation of effect of fluoride on corrosion of 2S-0 aluminum and 347 stainless steel in fuming nitric acid a t 170©� / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Charles E. Feiler, Gerald Morrell, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Some effects of fin plan form on the static stability of fin-body combinations at Mach number 4.06 / (Washington, D.C. : National Advisory Committee for Aeronautics, XXXX), by Edward F. Ulmann, Robert W. Dunning, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Aerodynamic characteristics of a canard-balanced, free-floating, all-movable stabilizer as obtained from rocket-powered-model flight tests and low-speed wind-tunnel tests / (Washington, D.C. : National Advisory Committee for Aeronautics, 1953), by William N. Gardner, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Three-degree-of-freedom evaluation of the longitudinal transfer functions of a supersonic canard missile configuration including changes in forward speed / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Ernest C. Seaberg, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Stability of two rocket-propelled models having aspect-ratio-5 unswept tails on a long body for the Mach number range of 1.7 to 2.4 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Reginald R. Lundstrom, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Nuclear powered lunar rockets / (Los Alamos, N.M. : Los Alamos Scientific Laboratory of the University of California, 1960), by Ralph S. Cooper, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
Wind tunnel tests of rectangular finned variable gap tangent ogive-cylinder model at Mach numbers 1.75 to 4.50 /, by Neil A. Zarin, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Wind tunnel magnus testing of a canted fin or self-rotating configuration /, by Anders S. Platou, U.S. Army Ballistic Research Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Compatibility of rocket propellants with materials of construction /, by Walter K Boyd, E. L. White, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
A time-dependent quasi-one-dimensional analysis of population inversions in an expanding gas /, by John D. Anderson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Flow visualization studies of a fin protuberance partially Immersed in a turbulent boundary layer at mach 5 /, by Allen E. Winkelmann and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Supersonic magnus measurements of the 10-Caliber Army-Navy spinner projectile with wrap-around fins /, by Frank J Regan, Virginia L. Schermerhorn, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
An experimental investigation of the laminar boundary layer on a spinning ogive cylinder in supersonic flow /, by William C. Ragsdale, Robert G. Ball, Michael A. Brown, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Basic material resulting from ANL rocket study / (Lemont, III. : Argonne National Laboratory, 1963), by C. Cohn, Argonne National Laboratory. ANL., and U.S. Atomic Energy Commission. ANL. (page images at HathiTrust)
Bibliography of books and published reports on gas turbines, jet propulsion, and rocket power plants / (Washington, D.C. : U.S. Dept. of Commerce, National Bureau of Standards, 1951), by Ernest Franklin Fiock, Carl Halpern, and United States. National Bureau of Standards. Circular (page images at HathiTrust)
Developing a payload for a high-altitude diagnostic rocket : mechanical engineering aspect / (Livermore, Ca. : Lawrence Radiation Laboratory, 1965), by Henry L. Knoll, John Harri, Karl Kiraly, United States. National Bureau of Standards. UC., United States. Department of Energy. Office of Fusion Energy. UC., United States. National Bureau of Standards. Fracture and Deformation Division. UC., United States. Energy Research and Development Administration. TID., U.S. Atomic Energy Commission. TID., and Lawrence Radiation Laboratory (page images at HathiTrust)
Tory II-A mechanical and aero-thermodynamic design / (Livermore, Ca. : [Lawrence] Radiation Laboratory, 1962), by J. W. Cox, United States. Energy Research and Development Administration. TID., U.S. Atomic Energy Commision. TID., and Livermore. Lawrence Radiation Laboratory University of California (page images at HathiTrust)
Stage optimization of the general multistage rocket / (Berkeley, Ca. : [Lawrence] Radiation Laboratory, 1961), by Robert H. Fox, United States. National Bureau of Standards. UC., United States. Department of Energy. Office of Fusion Energy Office of Fusion Energy. UC., United States. National Bureau of Standards. Facture and Deformation Division. UC., United States. Energy Research and Development Administration. TID., U.S. Atomic Energy Commision. TID., and Lawrence Radiation Laboratory (page images at HathiTrust)
Jane's all the world's aircraft, 1913 : a reprint of the 1913 edition of All the world's air-craft / (New York : Arco Publishing Co., 1969), ed. by Fred T. Jane (page images at HathiTrust)
Experimental investigation of a lightweight rocket chamber / (Washington, D.C. : National Advisory Committee for Aeronautics, [1953]), by John E. Dalgleish, Adelbert O. Tischler, United States. National Advisory Committee for Aeronautics. NACA research memorandum, United States. National Advisory Committee for Aeronautics, and Lewis Flilght Propulsion Laboratory (page images at HathiTrust)
Effect of fuel drop size and injector configuration on screaming in a 200-pound-thrust rocket engine using liquid oxygen and heptane / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Charles E. Feiler, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Investigation of an underslung half-cone inlet with compression surface mounted outboard from fuselage at mach numbers of 1.5, 1.8, and 2.0 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Richard A. Yeager, Laurence W. Gertsma, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Aerodynamic losses in low-pressure tailpipe exhaust ducts for rocket-propelled aircraft / (Washington, D.C. : National Advisory Committee for Aeronautics, 1948), by William K. Hagginbothom, J. G. Thibodaux, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Description and analysis of a rocket-vehicle experiment on flutter involving wing deformation and body motions / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by H. J. Cunningham, R. R. Lundstrom, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Langley 9-inch supersonic tunnel tests of several modifications of a supersonic missile having tandem cruciform lifting surfaces : three-component data results of models having ratios of wing span to tail span less than 1 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1960), by Robert W. Rainey, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Investigations at supersonic speeds of the base pressure on bodies of revolution with and without sweptback stabilizing fins / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Eugene S. Love, Robert M. O'Donnell, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Normal force, center of pressure, and zero-lift drag of several ballistic-type missiles at Mach numbers of 4.05 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Edward F. Ulmann, Robert W. Dunning, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Effects of some external-store mounting arrangements and store shapes on the buffet and drag characteristics of wingless rocket-powered models at Mach numbers from 0.7 to 1.4 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1954), by Homer P. Mason, Allen B. Henning, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Effects on adjacent surfaces from the firing of rocket jets / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Walter E. Bressette, Abraham Leiss, Langley Aeronautical Laboratory, United States. National Adviosry Committee for Aeronautics. NACA research memorandum, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1 / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Martin T. Moul, Andrew R. Wineman, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Sanford Gordon, Kenneth S. Drellishak, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Flight investigation at high-subsonic, transonic, and supersonic speeds to determine zero-lift drag of fin-stabilized bodies of revolution having fineness ratios of 12.5, 8.91, and 6.04 and varying positions of maximum diameter / (Washington, D.C. : National Advisory Committee for Aeronautics, 1949), by Roger G. Hart, Ellis R. Katz, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
Solution of a problem to obtain the optimum energy for a rocket initially in a circular orbit / (Los Alamos, N.M. : Los Alamos Scientific Laboratory of the University of California, 1960), by George A. Baker, John G. Wills, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
Preliminary investigation of the effects of several seeker-nose configurations on the longitudinal characteristics of a canard-type missile at a Mach number of 1.60 / (Washington : National Advisory Committee for Aeronautics, [1958]), by A. Warner Robins (page images at HathiTrust)
Characteristics of loads in rough air at transonic speeds of rocket-powered models of a canard and a conventional-tail configuration / (Washington [D.C.] : National Advisory Committee for Aeronautics, [1955]), by A. James Vitale and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Characteristics of the Nike-Cajun (CAN) rocket system and flight investigation of its performance / (Washington, D.C. : National Advisory Committee for Aeronautics, [1957]), by John F. Royall, Benjamine J. Garland, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Production of tungsten rocket nozzle inserts / (Oak Ridge, Tennessee : U.S. Atomic Energy Commission, Union Carbide Nuclear Company, 1961), by Arthur C. Neeley, Oak Ridge Y-12 Plant, Union Carbide Nuclear Company, and U.S. Atomic Energy Commission (page images at HathiTrust)
Re-entry flight demonstration number one (RFD-1) : Comparison of the preflight and observed trajectories / (Albuquerque, N. M. : Sandia Corporation, 1964), by H. R. Spahr and Sandia Corporation (page images at HathiTrust)
Flight investigation of a supersonic canard missile equipped with an auxiliary damping-in-pitch control system /, by Martin T. Moul, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
The Solar extreme ultraviolet spectrum between 30 March 1966 and 17 January 1967 /, by James E. Higgins and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Tests of long wire deployment from supersonic rockets /, by Charles B. Kalakowsky, Edward A. Lewis, George C. Hirst, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Attitude determination of a spinning and tumbling rocket using data from two orthogonal magnetometers /, by Shu T Lai and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Rocket-nozzle testing and evaluation /, by E. W Ungar and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
Design considerations in selecting materials for large solid-propellant rocket-motor cases /, by Charles Wesley Bert, Walter S. Hyler, Defense Metals Information Center (U.S.) issuing body, Battelle Memorial Institute. Defense Metals Information Center, and United States. Office of the Director of Defense Research and Engineering (page images at HathiTrust)
Fabrication of tungsten for solid-propellant rocket nozzles /, by Robert Isaac Jaffee, V. D. Barth, D. J. Maykuth, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
Compatibility of materials with rocket propellants and oxidizers /, by Walter K Boyd, E. L. White, Warren E. Berry, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
A time-dependent analysis for quasi-one-dimensional nozzle flows with vibrational and chemical nonequilibrium /, by John D. Anderson and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Flow field measurements around an ogive-cylinder at angles of attack up to 15 degrees for mach numbers 3.5 and 4 /, by William C. Ragsdale and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
The static and agnus aerodynamic characteristics of the M823 Research Store equipped with fixed and freely spinning stabilizers /, by Frank J Regan, Mary E. Falusi, and Md.) Naval Ordnance Laboratory (White Oak (page images at HathiTrust)
Wrap-around-fin (WAF) pressure distribution /, by John E. Holmes, Md.) Naval Ordnance Laboratory (White Oak, and Technical Cooperation Program (page images at HathiTrust)
Statistical techniques for describing localized vibratory environments of rocket vehicles / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], 1964), by Robert E. Barrett, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
An experimental investigation of the effect of gravity on a forced circulation pattern in spherical tanks / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Steven G. Berenyi, Kaleel L. Abdalla, Ralph C. Nussle, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Supersonic chemical propulsion feasibility flight demonstration for a low altitude short range missile., by Marquardt Corporation, R. R. Wells, and issuing body United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Effects of various exhaust blast deflectors on the acoustic noise characteristics of 1,000 pound-thrust rockets /, by John N. Cole, Robert G. Powell, Robert T. England, Aerospace Medical Laboratory. sponsor, sponsor United States. Wright Air Development Division, and United States. Air Force. Air Research and Development Command. issuing body (page images at HathiTrust)
Research on the feasibility of propellant detection by induced radioactive techniques /, by Frederick J. Brousaides, D. J. MacDonald, Carlton O. Hommel, James C. McCue, Richard Bersin, Inc. Tracerlab, sponsor Aerospace Medical Laboratory (U.S.), and issuing body United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Design, installation, and operation of an aerosol exposure chamber /, by Kenneth D. Johnson, sponsor Bionetics Research Laboratories, sponsor Atlantic Research Corporation, and sponsor Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
Toxicological studies on beryllium oxides and beryllium-containing exhaust products /, by Howard C. Spencer, Judith C. Jones, Salah E. Sadek, Susan B. McCollister, Judith A. Blumenshine, Robert H. Hook, sponsor Dow Chemical Company, and sponsor Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
Property determinations for CFW graphite /, by R. B. Dull, sponsor Air Force Materials Laboratory (U.S.), issuing agency United States. Air Force. Systems Command, and sponsor Union Carbide Corporation. Carbon Products Division (page images at HathiTrust)
Electroencephalographic and behavioral studies of monomethylhydrazine toxicity in the cat /, by M. B. Sterman, M. D. Fairchild, R. W. LoPresti, Los Angeles. School of Medicine University of California, and sponsor Aerospace Medical Research Laboratory (U.S.) (page images at HathiTrust)
The acute inhalation toxicity of monomethylhydrazine vapor /, by C. C. Haun, G. F. Egan, E. H. Vernot, J. D. MacEwen, and sponsor Aerospace Medical Research Laboratory (U.S.) (page images at HathiTrust)
Evaluation of the use of commercially available detectors for hydrazine and nitrogen dioxide of colorimetric dosimeters., by Robert F. Rakowski and sponsor Aerospace Medical Research Laboratory (U.S.) (page images at HathiTrust)
Toxicological studies on beryllium oxides and beryllium-containing exhaust products /, by Howard C. Spencer, Susan B. McCollister, Judith A. Blumenshine, Robert H. Hook, Judith C. Jones, Salah E. Sadek, sponsor Dow Chemical Company, and sponsor Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
Subconvulsive effects of monomethylhydrazine on runway performance in the cat /, by M. B. Sterman, H. B. van Twyver, M. D. Fairchild, and sponsor Aerospace Medical Research Laboratory (U.S.) (page images at HathiTrust)
The pressure-carbonization of carbon bonded silicon carbide-graphite for use in uncooled rocket nozzles /, by Telesphore L. Charland, Bruce R. Goss, James R. Tinklepaugh, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, and sponsor New York State College of Ceramics at Alfred University (page images at HathiTrust)
Bibliography of books and published reports on gas-turbines, jet propulsion, and rocket power plants / (Washington : U.S. Govt. Print. Off., 1949), by United States. National Bureau of Standards and Ernest F. Fiock (page images at HathiTrust; US access only)
High altitude rocket research / (New York, Academic Press, 1953), by Homer E. Newell (page images at HathiTrust)
Atoms, rockets, and the moon. (Los Angeles : Griffith Observatory, [1947]), by Dinsmore Alter (page images at HathiTrust; US access only)
A handbook of space flight (Chicago, Perastadion Press, 1950), by Wayne Arthur Proell and Norman J. Bowman (page images at HathiTrust)
Random vibration / (Cambridge, Mass. : M.I.T. Press, [1959, c1958]-1963), by Stephen H. Crandall (page images at HathiTrust)
Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4 / (Washington, D.C. : National Advisory Committee for Aeronautics, [1956]), by Earl D. Knechtel, Arvid N. Andrea, Ames Research Center, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Missile-site ground cover / (Vicksburg, Miss. : Waterways Experiment Station, 1973), by James W. Carr, Waterways Experiment Station (U.S.). Soils and Pavements Laboratory, and United States. Army Materiel Command (page images at HathiTrust)
Experimental aerodynamic forces and moments at low speed of a missile model during simulated launching from the midsemispan location of a 45 degree sweptback wing-fuselage combination /, by William J. Alford, Thomas J. King, H. Norman Silvers, Langley Aeronautical Laboratory, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
Summary of AFCRL rocket and satellite experiments (1946-1966) /, by A. McIntyre and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
A digital electronic data recording system for pulse-time telemetering /, by Gilbert O. Hall and Air Force Cambridge Research Center (U.S.). Geophysics Research Directorate, ed. by Robert M. Slavin (page images at HathiTrust)
Environmental safety aspects of nuclear rocket flight operations : annual progress report : for Space Nuclear Propulsion Office, Atomic Energy Commission, National Aeronautics and Space Administration. (Washington, D.C. : Nuclear Utility Services ; Oak Ridge, Tenn. : distributed by the U.S. Atomic Energy Commission, Division of Technical Information.), by U.S. Atomic Energy Commission. Division of Technical Information and United States. Space Nuclear Propulsion Office (page images at HathiTrust)
Estimation of performance factors for rocket propellants : a compilation of data from generalized systems and its application to specific propellant combinations /, by James Robert Muenger, Leonard Greiner, United States. Air Force. Systems Command. Rocket Research Laboratory, and Inc Texaco (page images at HathiTrust; US access only)
Studies on dynamics and instrumentation of the Holloman track /, by Air Force Missile Development Center (U.S.) and Knox Millsaps (page images at HathiTrust)
Final design of Sandia's supersonic parachute test vehicle / ([Albuquerque, N. M. ; Livermore, Calif. : Sandia National Laboratories ; Springfield, Va. : National Technical Information Service, 1960]), by M.T. Kane, B. L. Barth, and Sandia Corporation (page images at HathiTrust)
An economical, lightweight, foamed fin for rocket application / ([Albuquerque, N.M.] : Sandia Corporation ; Washington, D.C. : Available from the Office of Technical Services, Department of Commerce, [1961]), by T. M. Sedgwick and Sandia Corporation (page images at HathiTrust; US access only)
Radio-frequency attenuation measurements on high altitude nuclear detonations / (Albuquerque, N.M. : Sandia Corporation, Technical Information Division ; Washington, D.C. : Available from the Office of Technical Services, Dept. of Commerce, 1960), by J. L. Dossey and Sandia Corporation (page images at HathiTrust)
Rocket optical observation of a day-time aurora /, by S. M. Silverman, L. J. Nardone, B. L. Cochrun, John W. F. Lloyd, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Rocket spectra of the chromosphere /, by H. E. Hinteregger and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Distribution of ROBIN sensed wind shears at 30 to 70 kilometers /, by Henry A. Salmela, Norman Sissenwine, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
Potentials and charges on conducting rocket sections /, by Charles W. Dubs and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
Research on materials and methods for decontamination of toxic missile propellant spillage /, by J. M. Siegmund, B. T. Poon, R. E. Ogden, R. B. Jackson, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Allied Chemical Corporation (page images at HathiTrust)
Amperometric propellent-component detector /, by Nicholas A. Poulos, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Olin Mathieson Chemical Corporation (page images at HathiTrust)
Studies of rocket noise simulation with substitute gas jets and the effect of vehicle motion on jet noise /, by Walter V. Morgan, Kenneth J. Young, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Boeing Company (page images at HathiTrust)
Orbital maneuvers with finite thrust rockets /, by Robert W. Roig and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Evaluation of elastomers as o-ring seals for liquid rocket fuel and oxidizer systems /, by Carmen L. Bellanca, Jay C. Harris, Ival O. Salyer, issuing body United States. Air Force. Systems Command. Research and Technology Division, sponsor Air Force Materials Laboratory (U.S.), and sponsor Dayton Laboratory (page images at HathiTrust)
Far field noise and vibration levels produced during the Saturn SA-1 launch : (Preliminary report) /, by J. N. Cole, C. E. Thomas, sponsor Aerospace Medical Research Laboratories (U.S.), and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
Distribution and excretion of ¹⁴C-monomethylhydrazine /, by Mildred K. Pinkerton, Kenneth C. Back, Edgar A. Hagan, and sponsor Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
Calculation of the specific impulse of rocket propellants /, by Rudolph Edse and issuing agency United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
The use of digital techniques for flight control; a discussion prepared for SAE Committee A-18 on Aerospace Vehicle Flight Control Systems. ([Buffalo] Cornell Aeronautical Laboratory, Flight Research Dept., 1961), by J. Norman Ball (page images at HathiTrust)
The magnetic induction plasma engine. (Los Angeles, Physical Research Laboratory, Space Technology Laboratories, 1960), by Milton U. Clauser (page images at HathiTrust)
The application of short-duration techniques to the experimental study of base heating (Buffalo, Cornall Aeronautical Laboratory, Inc., 1961), by K. D. Bird (page images at HathiTrust)
Characterization of the flowfield near a wrap-around fin at supersonic speeds /, by Carl P. Tilmann and Ohio). Air Vehicles Directorate Air Force Research Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
An analytical study of hypersonic inlets in free-molecule flow /, by M. Kinslow, M. R. Busby, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
Aerodynamic characteristics of low aspect ratio fins at Mach numbers from 0.80 to 1.30 /, by D.K. Smith, R. C. German, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Environmental pollution by missile propellants /, by Walter W. Heck, Martha B. Porter, Dale R. Darling, William J. Clark, Morris E. Bloodworth, Luther S. Bird, sponsor Wright-Patterson Air Force Base (Ohio), sponsor Texas A & M Research Foundation, and issuing body Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
High alpha aerodynamics /, by Inc ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Aerodynamic characteristics of several low aspect ratio stabilizer fins at Mach numbers from 0.8 to 1.3 /, by J. M. Whoric, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
A compilation of static stability and fin loads data for slender body missile models with and without tail fins and wings., by G. R. Gomillion, sponsor Air Force Armament Laboratory (U.S.), Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
Static aerodynamic characteristics of a series of generalized slender bodies with and without fins at Mach numbers form 0.6 to 3.0 and angles of attack from 0 to 180 deg., by William B. Baker, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
The Dynamics of spinning bodies at large angle of attack /, by J. E. Brunk, R. W. Rakestraw, W. L. Davidson, and United States. Air Force. Office of Scientific Research. issuing body (page images at HathiTrust)
Vortex induced rolling moments on finned missiles at high angle of attack /, by Daniel G. Udelson, issuing body United States. |b Air Force. |b Systems Command, sponsor Air Force Cambridge Research Laboratories (U.S.), and sponsor Boston University (page images at HathiTrust)
Vortex induced rolling moments on cruciform missiles at high angle of attack /, by Steven I. Kane, issuing body United States. |b Air Force. |b Systems Command, sponsor Air Force Cambridge Research Laboratories (U.S.), and sponsor Boston University (page images at HathiTrust)
Estimated noise produced by large space vehicles as related to establishing tentative safe distances to adjacent launch pads and the community /, by John N. Cole, Robert G. Powell, and sponsor Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
An investigation of vortex path and strength of finned missiles at high angle of attack and numerical calculation of induced rolling moment /, by Charles S. W. Wong, issuing body United States. |b Air Force. |b Systems Command, sponsor Air Force Cambridge Research Laboratories (U.S.), and sponsor Boston University (page images at HathiTrust)
Aerodynamic and cold jet plume geometry characteristics of the Army free rocket at transonic mach numbers /, by E. S. Washington, Inc. sponsor ARO, United States. Air Force. Arnold Air Force Base. sponsor, and United States. Air Force. Systems Command. Arnold Engineering Development Center. issuing body (page images at HathiTrust)
A comparative analysis of convective heat transfer in a nuclear rocket nozzle / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Harvey E. Neumann, Paula J. Bettinger, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Simulator study of a satellite attitude control system using inertia wheels and a magnet / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by James J. Adams, Hugh P. Bergeron, W. E. Howell, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
Erosion resistance and failure mechanisms of several nozzle materials in a small solid-propellant rocket engine / (Washington, D.C. : National Aeronautics and Space Administration, 1963), by Robert A. Signorelli, James R. Johnston, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

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