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Noses (Space vehicles)

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• Space vehicles

• Noses (Space vehicles) -- Aerodynamics
• Noses (Space vehicles) -- Design and construction
• Noses (Space vehicles) -- Mathematical models
• Noses (Space vehicles) -- Models
• Noses (Space vehicles) -- Research
• Noses (Space vehicles) -- Testing

• Nose cones (Space vehicles)
• Space vehicles -- Nose cones

• Surface roughness of ablated carbon-carbon nosetip composites (Air Force Materials Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978), by Julius Jortner (page images at HathiTrust)
• Optimum shape for transpiration-cooled nosetip of a re-entry vehicle (Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978), by Kevin E. Yelmgren (page images at HathiTrust)
• Measured and predicted shock shapes and aerodynamic coefficients for blunted cones at incidence in helium at Mach 20.3 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), by Robert L. Calloway, Nancy H. White, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• NASA TN D-2163 (National Aeronautics and Space Administration :, 1964), by John T. Suttles, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-2201 (National Aeronautics and Space Administration :, 1964), by J. Wayne Keyes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Attached and separated boundary layers on highly cooled, ablating and nonablating models at M=13.8 (National Aeronautics and Space Administration ;, 1967), by Donald M. Kuehn and Daryl J. Monson (page images at HathiTrust)
• NASA TN D-5766 (National Aeronautics and Space Administration :, 1970), by Michael C. Fischer, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4800 (National Aeronautics and Space Administration :, 1968), by Charles G. Miller and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5341 (National Aeronautics and Space Administration ;, 1969), by John V. Rakich, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-4961 (National Aeronautics and Space Administration ;, 1969), by P. Calvin Stainback, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4713 (National Aeronautics and Space Administration ;, 1968), by Randolph A. Graves, William G. Witte, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A theoretical and experimental study of hypersonic flow over flared bodies at incidence (National Aeronautics and Space Administration ;, 1966), by John V. Rakich, Gene P. Menees, and Ames Research Center (page images at HathiTrust)
• Development of an analytic model of the response of self-contained, transpiration-cooled nose tips to reentry environments (Albuquerque, New Mexico : Sandia Corporation, Aero-Thermodynamics Department, 1968., 1968), by I. M. Grinberg, E. W. Ungar, W. H. Lane, G. R. Whitacre, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Summary of static stability and drag characteristics of axisymmetric low-drag shapes for the subsonic to hypersonic mach number range (Albuquerque, New Mexico : Sandia Laboratories, Experimental Aerodynamics Laboratories, 1968., 1968), by Amado A. Trujillo, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)
• Handbook of inviscid sphere-cone flow fields and pressure distributions (White Oak, Silver Spring, Marlyand : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by A. M. Morrison, Naval Surface Weapons Center. White Oak Laboratory, R. E. Ferguson, M. Ciment, and J. M. Solomon (page images at HathiTrust)
• An Investigation of the damping in pitch characteristics of a ten degree cone (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by A. M. Morrison, W. R. Lawrence, J. E. Holmes, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Effect of nose diameter on the erosion of spherical nosetip reentry bodies (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1976., 1976), by Jr. Sheetz, John E. Holmes, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Two-component force balance for measuring skin friction and side force (Silver Spring, Maryland : Naval Surface Weapons Center, White Oak Laboratory, 1975., 1975), by Eugene V. Horanoff, Richard T. Driftmyer, and Naval Surface Weapons Center. White Oak Laboratory (page images at HathiTrust)
• Performance of a microwave antenna system in the shoulder region of a blunt reentry nose cone (Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973), by J. Leon Poirier, David H. Tropea, John D. Antonucci, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• Heat transfer correlations for blunt cones at angle of attack (Los Angeles, California : Space and Missile Systems Organization, Air Force Systems Command, United States Air Force, 1971., 1971), by George F. Widhopf, United States. Air Force. Systems Command, Space and Missile Systems Organization (U.S.), and Aerospace Corporation (page images at HathiTrust)
• Boundary layer transition at supersonic speeds : three dimensional roughness effects (spheres) (Washington, D.C. : Air Force Office of Scientific Research, United States Air Force, 1961., 1961), by E. R. Van Driest, C. B. Blumer, United States. Air Force. Office of Scientific Research, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Heat-transfer and shadowgraph tests of several elliptical lifting bodies at Mach 10 (Arnold Air Force Station, Tennessee : Arnold Engineering Development Center, Air Force Systems Command, United States Air Force, 1964., 1964), by M. E. Hillsamer, J. P. Rhudy, Inc ARO, Arnold Engineering Development Center, and United States. Air Force. Systems Command (page images at HathiTrust)

• Subsonic and supersonic static aerodynamic characteristics of a family of bulbous base cones measured with a magnetic suspension and balance system (National Aeronautics and Space Administration ;, 1972), by Milan Vlajinac, Langley Research Center, and Massachusetts Institute of Technology (page images at HathiTrust)
• NASA TR R-117 (National Aeronautics and Space Administration :, 1961), by Donald M. Kuehn and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5201 (National Aeronautics and Space Administration ;, 1969), by Robert J. McGhee, W. Frank Staylor, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1781 (National Aeronautics and Space Administration ;, 1963), by David S. Shaw, C. Donald Babb, Dennis E. Fuller, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri. (National Aeronautics and Space Administration :, 1962), by Peter F. Intrieri and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wind-tunnel investigation at mach numbers from 0.30 to 1.14 of the static aerodynamic characteristics of modified Mercury escape and exit capsule configurations (National Aeronautics and Space Administration, 1961), by Albin O. Pearson and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Predicted gas properties in the shock layer ahead of capsule-type vehicles at angles of attack (National Aeronautics and Space Administration, 1962), by George E. Kaattari and Ames Research Center (page images at HathiTrust)

• Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri. (National Aeronautics and Space Administration :, 1962), by Peter F. Intrieri and United States National Aeronautics and Space Administration (page images at HathiTrust)

• NASA TN D-4598 (National Aeronautics and Space Administration ;, 1968), by George C. Ashby, W. Frank Staylor, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Comparison of predicted and experimental real-gas pressure distributions on Space Shuttle Orbiter nose for Shuttle Entry Air Data System (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1980), by Judy L. Shinn, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A parametric study of the aerodynamic characteristics of nose-cylinder-flare bodies at a Mach number of 6.0 (National Aeronautics and Space Administration ;, 1965), by George C. Ashby, Aubrey M. Cary, and Langley Research Center (page images at HathiTrust)
• Dynamic model tests at low subsonic speeds of Project Mercury capsule configurations with and without drogue parachutes (National Aeronautics and Space Administration, 1961), by James S. Bowman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Test plan optimization for reentry vehicle nose tip evaluation (Albuquerque, New Mexico : Sandia Corporation, Aero-Thermodynamics Department, 1967., 1967), by Roald A. Rindal, Thomas J. Dahm, U.S. Atomic Energy Commission, and Sandia Corporation (page images at HathiTrust)

Items below (if any) are from related and broader terms.

• Mezhplanetnsi︠a︡ sreda i fizika atmosfery (National Aeronautics and Space Admin., 1974), by Gennadiĭ Aleksandrovich Skuridin (page images at HathiTrust)
• Aero-space applied thermodynamics manual. (Society of Automotive Engineers, Committee A-9: Aero-space Environmental Control Systems, 1962), by Society of Automotive Engineers (page images at HathiTrust)
• Fundamentals of rockets, missiles, and spacecraft (J.F. Rider, 1962), by Marvin Hobbs (page images at HathiTrust; US access only)
• Principles of bioastronautics. (Prentice-Hall, 1963), by Siegfried J. Gerathewohl (page images at HathiTrust)
• International missile and spacecraft guide (McGraw-Hill, 1960), by Frederick I. Ordway and Ronald C. Wakeford (page images at HathiTrust)
• Radio frequency control in space telecommunications. Prepared at the request of Lyndon B. Johnson, chairman, for the use of the Committee on Aeronautical and Space Sciences, United States Senate (U. S. Govt. Print. Off., 1960), by Library of Congress Legislative Reference Service, E. Wenk, and United States. Congress. Senate. Committee on Aeronautical and Space Sciences (page images at HathiTrust)
• Aeroassist, key to returning from space and the case for AFE (National Aeronautics and Space Administration, 1991), by Louis J. Williams, Terrill W. Putnam, Robert Morris, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Space Division : a chronology, 1980 - 1984 (Office of History, Headquarters, 1991), by J. Catherene Wilman and United States. Air Force. Space Division. Office of History (page images at HathiTrust)
• Space shuttle accident hearings before the Subcommittee on Science, Technology, and Space of the Committee on Commerce, Science, and Transportation, United States Senate, Ninety-ninth Congress, second session, on space shuttle accident and the Rogers Commission report, February 18, June 10, and 17, 1986. (U.S. G.P.O., 1986), by Science United States. Congress. Senate. Committee on Commerce (page images at HathiTrust)
• Space transportation system hearings (including report) before the Subcommittee on Space Science and Applications of the Committee on Science and Technology, U.S. House of Representatives, Ninety-fifth Congress, first session, May 17, 18, 1977. (U.S. Govt. Print. Off., 1977), by United States. Congress. House. Committee on Science and Technology. Subcommittee on Space Science and Applications (page images at HathiTrust)
• Space shuttle operational planning, policy, and legal issues hearings before the Subcommittee on Space Science and Applications of the Committee on Science and Technology, U.S. House of Representatives, Ninety-sixth Congress, first session, September 25, 26, 1979. (U.S. Govt. Print. Off., 1979), by United States. Congress. House. Committee on Science and Technology. Subcommittee on Space Science and Applications (page images at HathiTrust)
• Magellan. (National Aeronautics and Space Administration :, 1985), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• A note on importance functions for the shielding of manned space vehicles (Oak Ridge National Laboratory, 1964), by R. G. Jr Alsmiller and U.S. Atomic Energy Commission (page images at HathiTrust)
• Space measurements survey: Instruments and spacecraft, October 1957-March 1965. (Scientific and Technical Information Division, National Aeronautics and Space Administration, 1966), by Henry L. Richter, United States National Aeronautics and Space Administration, and Electro-Optical Systems (Firm) (page images at HathiTrust)
• Spacecraft for radar propagation experiments; design study progress report. (Buffalo, 1962), by Cornell Aeronautical Laboratory, C. L. Meese, and C. L. Muzzey (page images at HathiTrust)
• Fundamentals of [aircraft and missile] structures (Air Science Associates of Southern California for the U. S. Air Force Institute of Technology, Wright-Patterson Air Force Base, 1960), by Hugh Harrison Hurt (page images at HathiTrust)
• Quarterly progress report on a study of meteoroid impact phenomena (Cornell Aeronautical Laboratory, Inc., 1962), by William Joseph Rae and Henry Paul Kirchner (page images at HathiTrust)
• Outer-space environment models for use with space vehicle simulators. (Behavioral Sciences Laboratory, Aerospace Medical Research Laboratories, Aerospace Medical Division, Air Force Systems Command, 1961), by William A. Livingston (page images at HathiTrust)
• An analysis and procedure for determining space environmental sink temperatures with selected computational results (National Aeronautics and Space Administration, Lewis Research Center, 2001), by Albert J. Juhasz and Lewis Research Center (page images at HathiTrust)
• NASA standard procedures for the microbiological examination of space hardware. (National Aeronautics and Space Administration : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1980), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• A New dimension in space experimentation : LDEF. (National Aeronautics and Space Administration :, 1984), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cosmic background explorer (National Aeronautics and Space Administration, Goddard Space Flight Center, 1986), by John C. Mather, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The International Cometary Explorer (ICE) wallsheet : teacher's guide (National Aeronautics and Space Administration, Goddard Space Flight Center ;, 1985), by Stephen P. Maran and Goddard Space Flight Center (page images at HathiTrust)
• Space transportation : NASA has no firm need for increasingly costly Orbital Maneuvering Vehicle : report to the Chairman, Committee on Science, Space, and Technology, House of Represenatives (The Office, 1990), by United States General Accounting Office and Space United States. Congress. House. Committee on Science (page images at HathiTrust)
• Aerospace plane technology : research and development efforts in Europe (United States General Accounting Office, 1991), by United States General Accounting Office and United States. General Accounting Office. National Security and International Affairs Division (page images at HathiTrust)
• Designating and naming defense military aerospace vehicles : operations support. (Secretaries of the Air Force, Army, and Navy, 1997), by United States. Dept. of the Air Force (page images at HathiTrust)
• The Soviet space challenge. (Dept. of Defense, 1987), by United States. Dept. of Defense (page images at HathiTrust)
• Effects of relaxed static longitudinal stability on a single-stage-to-orbit vehicle design (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), by Delma C. Freeman, Alan W. Wilhite, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Purging of a multilayer insulation with Dacron tuft spacer by gas diffusion (National Aeronautics and Space Administration ;, 1976), by Irving E. Sumner, William J. Fisk, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Space shuttle pogo active controller design using frequency domain optimization (U.S. National Aeronautics and Space Administration ;, 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)
• Single launch lunar habitat derived from NSTS external tank (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), by Charles B. King and Langley Research Center (page images at HathiTrust)
• Global matrix of thermospheric density values for selected solar/geomagnetic conditions and spacecraft orbital altitudes (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), by D. L. Johnson and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Environmental analysis of the Chemical Release Module program (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), by James P. Heppner, Maurice Dubin, Goddard Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Performance of a Haynes 188 metallic standoff thermal protection system at Mach 7 (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Don E. Avery, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Empirically determined wind and scale effects on hot gas recirculation characteristics of jet V/Stol aircraft (National Aeronautics and Space Administration, 1969), by Patrick E. Ryan, Wayne J. Cosgrove, Bell Aerospace Corporation. Bell Aerosystems Company, and Langley Research Center (page images at HathiTrust; US access only)
• Deployable centrifugally stabilized structures for atmospheric entry from space (National Aeronautics and Space Administration :, 1964), by H. U. Schuerch, R. MacNeal, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Terrestrial environment (climatic) criteria guidelines for use in space vehicle development, 1969 revision (National Aeronautics and Space Administration, 1969), by Glenn E. Daniels and George C. Marshall Space Flight Center (page images at HathiTrust)
• The use of man in booster guidance and control (National Aeronautics and Space Administration, 1964), by F. A. Muckler and R. W. Obermayer (page images at HathiTrust; US access only)
• Design and application of polycarbonate capacitors in aerospace AC power systems (National Aeronautics and Space Administration :, 1971), by J. F. Gosda, R. R. Bailey, A. C. Elles, Lewis Research Center, United States National Aeronautics and Space Administration, and TRW Inc (page images at HathiTrust)
• Narrow band cross-correlation analysis of fluctuating pressures beneath a turbulent boundary layer (National Aeronautics and Space Administration, 1968), by C. M. Ailman and A. S. Hopkins (page images at HathiTrust; US access only)
• Passive geodetic satellite canister assemblies (National Aeronautics and Space Administration, 1967), by James O. Gibson and Robert R. Carman (page images at HathiTrust; US access only)
• Maintainability of manned spacecraft for long-duration flights. Volume 1 - Summary report. (National Aeronautics and Space Administration ;, 1968), by Ames Research Center, Boeing Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Filament-reinforced composites for aerospace structural applications. (National Aeronautics and Space Administration, 1965), by Norris F. Dow, B. Walter Rosen, General Electric Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thin sheet impact (National Aeronautics and Space Administration, 1965), by C. J. Maiden, R. E. Sennett, and A. R. McMillan (page images at HathiTrust; US access only)
• Effects and importance of penetration and growth of lift on space vehicle response (National Aeronautics and Space Administration, 1965), by Robert R. Blackburn and A. D. St. John (page images at HathiTrust; US access only)
• Optimum earth re-entry corridors (National Aeronautics and Space Administration, 1966), by Ann Muzyka and Elmore H. Blanton (page images at HathiTrust; US access only)
• Linear aerodynamic loads on cone-cylinders at Mach numbers from 0.7 to 2.0 (National Aeronautics and Space Administration, 1966), by Roger Lee Hamner and Alan D. Leff (page images at HathiTrust; US access only)
• A computer program for calculating the charge distribution about a space vehicle (National Aeronautics and Space Administration, 1966), by Lee W. Parker (page images at HathiTrust; US access only)
• Evaluation of self-sealing structures for space vehicle application (National Aeronautics and Space Administration, 1966), by Philip J. D'Anna and Roger M. Heitz (page images at HathiTrust; US access only)
• An experimental study of liquid surface oscillations in longitudinally excited compartmented cylindrical and spherical tanks (National Aeronautics and Space Administration, 1966), by Daniel D. Kana (page images at HathiTrust; US access only)
• Minimax control of large launch boosters (National Aeronautics and Space Administration, 1966), by K. D. Graham (page images at HathiTrust; US access only)
• Analysis of an optimal celestial-inertial navigation concept for low-thrust interplanetary vehicles (National Aeronautics and Space Administration, 1966), by Alan L. Friedlander (page images at HathiTrust; US access only)
• Design considerations for thermostatic fin spacecraft temperature control (National Aeronautics and Space Administration, 1966), by J. A. Wiebelt, G. J. Kneissl, and C. A. Morgan (page images at HathiTrust; US access only)
• Experimental study of acoustic displays of flight parameters in a simulated aerospace vehicles (National Aeronautics and Space Administration, 1966), by Darryl Katz (page images at HathiTrust; US access only)
• Convective and radiative heat transfer during superorbital entry (National Aeronautics and Space Administration, 1966), by H. Hoshizaki and K. H. Wilson (page images at HathiTrust; US access only)
• Investigation of three classes of composite materials for space vehicle application (National Aeronautics and Space Administration, 1967), by John A. Alexander, B. A. Macklin, and J. C. Withers (page images at HathiTrust; US access only)
• Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique (U.S. National Aeronautics and Space Administration ;, 1976), by Frank Marconi, Larry Yaeger, Manuel Salas, United States National Aeronautics and Space Administration, and Grumman Aerospace Corporation (page images at HathiTrust)
• Technology requirements for advanced earth-orbital transportation systems : summary report (National Aeronautics and Space Administration ;, 1977), by Rudolph C. Haefeli, Langley Research Center, Martin Marietta Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Summary report of evaluation of coated columbium alloy heat shields for space shuttle thermal protection system application (National Aeronautics and Space Administration ;, 1977), by W. E. Black, General Dynamics Corporation. Convair Division, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Cryogenic performance of slotted brazed Rene ́41 honeycomb panels (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1982), by Andrew K. Hepler, Allan R. Swegle, Langley Research Center, Boeing Aerospace Company, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Feasibility, parametric design, and comparative analysis of an unguided solid fuel rocket vehicle with solar orbit, earth probe, and re-entry mission capabilities (National Aeronautics and Space Administration, 1967), by T. C. Walker (page images at HathiTrust; US access only)
• Analytical study of impact effects as applied to the meteoroid hazard (National Aeronautics and Space Administration, 1967), by R. L. Bjork, M. H. Wagner, and K. N. Kreyenhagen (page images at HathiTrust; US access only)
• Tables of aerodynamic coefficients obtained from developed Newtonian expressions for complete and partial conic and spheric bodies at combined angles of attack and sideslip with some comparisons with hypersonic experimental data (U.S. G.P.O., 1962), by William R. Wells, William O. Armstrong, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Study of an automatic system for control of the terminal phase of satellite rendezvous (U.S. G.P.O., 1962), by Edgar C. Lineberry, Edwin C. Foudriat, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Study of an automatic system for control of the terminal phase of satellite rendezvous (U.S. G.P.O., 1962), by Edgar C. Lineberry, Edwin C. Foudriat, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• NASA TR R-362 (National Aeronautics and Space Administration ;, 1971), by Thomas W. Flatley, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The attainability of heavenly bodies (National Aeronautics and Space Administration, 1960), by Walter Hohmann and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A preliminary study of the use of finite-thrust engines for abort during launch of space vehicles (National Aeronautics and Space Administration :, 1961), by William A. McGowan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance evaluation of a two-dimensional ion rocket using through-feed and porous tungsten ionizers. (National Aeronautics and Space Administration :, 1961), by David L. Lockwood, Ronald J. Cybulski, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Discussions of solar proton events and manned space flight (National Aeronautics and Space Administration :, 1961), by Kinsey A. Anderson, Carl E. Fichtel, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Ultraviolet astronomical photometry from rockets (National Aeronautics and Space Administration :, 1962), by Albert Boggess and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Two-dimensional ion beams with small lateral spreading (National Aeronautics and Space Administration :, 1961), by Harold Mirels and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of systems using inertia wheels for precise attitude control of a satellite (National Aeronautics and Space Administration :, 1961), by John S. White, Q. Marlon Hansen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Loads induced on a flat-plate wing by an air jet exhausting perpendicularly through the wing and normal to a free-stream flow of mach number 2.0 (National Aeronautics and Space Administration :, 1961), by Joseph J. Janos and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-2357 (National Aeronautics and Space Administration :, 1964), by Keung P. Luke, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Contributions of rockets and satellites to the world magnetic survey (National Aeronautics and Space Administration :, 1961), by James P. Heppner, Joseph C. Cain, Thomas L. Skillman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The Arctic meteorology photo probe (National Aeronautics and Space Administration :, 1962), by Harold E. Evans, Andryshak. Richard J., Robert C. Baumann, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-2464 (National Aeronautics and Space Administration :, 1964), by Alan Arias, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust; US access only)
• NASA TN D-2489 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by James P. Arrington, Arthur Henderson, Roy C. Joiner, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-2498 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1964), by Demo J. Giulianetti, Victor R. Corsiglia, James C. Biggers, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-3760 (National Aeronautics and Space Administration ;, 1967), by Robert N. Lea, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-3732 (National Aeronautics and Space Administration [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1966), by James E. Love, William R. Young, Flight Center Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3733 (National Aeronautics and Space Administration [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1967), by Walter H. Kohl, R. W. Wilmarth, C. M. Veronda, Electronics Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gravity torque on an orbiting vehicle (National Aeronautics and Space Administration, 1959), by B. F. Doolin and Ames Research Center (page images at HathiTrust)
• A preliminary study of a solar-probe mission (National Aeronautics and Space Administration :, 1961), by Duane W. Dugan and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Piloted simulator tests of a guidance system which can continuously predict landing point of a low L/D vehicle during atmosphere re-entry (National Aeronautics and Space Administration :, 1961), by Rodney C. Wingrove, Robert E. Coate, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3578 (National Aeronautics and Space Administration :, 1966), by Alan D. Sherer and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Important research problems in missile and spacecraft structural dynamics : M.V. Barton. (National Aeronautics and Space Administration :, 1962), by Millard V. Barton and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of high-speed-impact attenuation by gas bags John Thomas Howe. (National Aeronautics and Space Administration :, 1962), by John Thomas Howe and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Survey of energy-absorption devices for soft landing of space vehicles (National Aeronautics and Space Administration :, 1962), by Jack B. Esgar and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3466 (National Aeronautics and Space Administration ;, 1966), by W. B. Fichter, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5283 (National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by J. H. Boeckel, A. R. Timmins, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Observations of properties of sintered wrought tungsten sheet at very high temperatures (National Aeronautics and Space Administration :, 1963), by Earl C. Sutherland, William D. Klopp, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed longitudinal aerodynamic characteristics associated with a series of low-aspect-ration wings having variations in leading contour / Bernard Spencer Jr. and Alexander D. Hammond. (National Aeronautics and Space Administration :, 1962), by Bernard Spencer, Alexander D. Hammond, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static longitudinal stability and performance of several ballistic spacecraft configuration in helium at a Mach number of 24.5 (National Aeronautics and Space Administration :, 1962), by Patrick J. Johnston, Curtis D. Snyder, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of some typical geometrical constraints on lunar trajectories (National Aeronautics and Space Administration :, 1961), by Robert H. Tolson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landing characteristics of a lentiucular-shaped reentry vehicle (National Aeronautics and Space Administration :, 1961), by Ulysse J. Blanchard and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of shield positioni and absorptivity on temperature distribution of a body shielded from solar radiation in space (National Aeronautics and Space Administration :, 1961), by Lester D. Nichols and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4416 (National Aeronautics and Space Administration ;, 1968), by R. James Rollbuhler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Efflux of thermal radiation from a cylindrical cavity irradiated from an external source (National Aeronautics and Space Administration :, 1962), by Ephraim M. Sparrow and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lunar trajectories (National Aeronautics and Space Administration :, 1961), by Richard J. Weber, Richard R. Burley, Werner M. Pauson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Results from a rocket-borne Langmuir probe experiment (National Aeronautics and Space Administration :, 1961), by Gideon P. Serbu and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of an active control system for a spinning body (National Aeronautics and Space Administration :, 1961), by James J. Adams and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The simultaneous measurement of ionospheric electron densities by CW propagation and RF impedance probe techniques (National Aeronautics and Space Administration :, 1962), by J. A. Kane, H. A. Whale, J. E. Jackson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The design of various types of air bearing for stimulating frictionless environments (National Aeronautics and Space Administration, 1962), by Kenneth W. Stark, United States National Aeronautics and Space Administration, and Goddard Space Flight Center (page images at HathiTrust)
• Apollo experience report; engineering and analysis, mission support (National Aeronautics and Space Administration, 1975), by Robert W. Fricke (page images at HathiTrust)
• A spacecraft-borne gradiometer mission analysis (U.S. National Aeronautics and Space Administration ;, 1976), by P. Argentiero, R. Garza-Robles, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landing-impact characteristics of load-alleviating struts on a model of a winged space vehicle (National Aeronautics and Space Administration :, 1960), by Ulysse J. Blanchard and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6109 (National Aeronautics and Space Administration:, 1971), by W. Thomas Blackshear (page images at HathiTrust; US access only)
• Interaction of highly underexpanded jets with simulated lunar surfaces (National Aeronautics and Space Administration :, 1961), by Leonard E. Stitt and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Attitude reacquisition of a gravity-gradient control-moment-gyro stabilized spacecraft. (National Aeronautics and Space Administration :, 1970), by Clark E. Stohl, Bruce E. LeRoy, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Shock interference heat transfer to tank configurations mated to a straight-wing space shuttle orbiter at mach number 10.3 (National Aeronautics and Space Administration ;, 1976), by Davis H. Crawford, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• A simplified analytical solution for thermal response of a one-dimensional, steady-state transpiration cooling system in radiative and convective environment (National Aeronautics and Space Administration ;, 1976), by Hirotoshi Kubota and Ames Research Center (page images at HathiTrust)
• NASA TN D-5864 (National Aeronautics and Space Administration ;, 1970), by Otto F. Trout, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5775 (National Aeronautics and Space Administration :, 1970), by Bernhard Dorsch, Warner H. Miller, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• An integrated circuit floating point accumulator (National Aeronautics and Space Administration ;, 1977), by Theodore C. Goldsmith and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Attitude control of a spacecraft with a strapdown inertial reference system and onboard computer (National Aeronautics and Space Administration :, 1970), by John Hrastar, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5991 (National Aeronautics and Space Administration :, 1970), by Charles L. Younger, Gilbert N. Wrights, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental evaluation of a breadboard heat and product-water removal system for a space-power fuel cell designed with satic water removal and evaporative cooling (National Aeronautics and Space Administration ;, 1977), by Norman H. Hagedorn, Paul R. Prokopius, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6000 (National Aeronautics and Space Administration ;, 1970), by Margaret M. Smith, Lewis Research Center, United States National Aeronautics and Space Administration, and Charles C. Giamati (page images at HathiTrust; US access only)
• NASA TN D-5032 (National Aeronautics and Space Administration ;, 1969), by Julian L. Jenkins, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Apollo ablator thermal performance at superorbital entry velocities (National Aeronautics and Space Administration :, 1970), by Donald M. Curry, Emily W. Stephens, Manned Spacecraft Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4849 (National Aeronautics and Space Administration :, 1968), by James E. Vrancik, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-4843 (National Aeronautics and Space Administration :, 1968), by Bobby L. Berrier, Odis C. Pendergraft, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-4848 (National Aeronautics and Space Administration :, 1968), by Steven V. Szabo, Andrew J. Stofan, James A. Berns, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5340 (National Aeronautics and Space Administration ;, 1969), by Thomas W. Orange, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5362 (National Aeronautics and Space Administration ;, 1969), by Edward P. Phillips, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5678 (National Aeronautics and Space Administration :, 1970), by Daniel J. Lesco, William C. Nieberding, John C. Sturman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5696 (National Aeronautics and Space Administration ;, 1970), by George F. Sykes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5341 (National Aeronautics and Space Administration ;, 1969), by John V. Rakich, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5345 (National Aeronautics and Space Administration ;, 1969), by John Zuk, Lawrence P. Ludwig, Patricia J. Smith, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5682 (National Aeronautics and Space Administration ;, 1970), by Henry A. Putre, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-6626 (National Aeronautics and Space Administration :, 1972), by John M. Jerke, Robert J. Platt, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Launch window analysis in a new perspective with examples of departures from earth to Mars (National Aeronautics and Space Administration, 1972), by Joseph R. Thibodeau, Victor R. Bond, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6719 (National Aeronautics and Space Administration :, 1972), by Michael J. Rutkowski, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo 9 thermal-control-coating degradation (National Aeronautics and Space Administration ;, 1972), by James A. Smith and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Flow-field measurements around a Mars lander model using hot-film anemometers under simulated Mars surface conditions (National Aeronautics and Space Administration ;, 1972), by George C. Greene and Langley Research Center (page images at HathiTrust)
• A digital solar aspect sensor (National Aeronautics and Space Administration :, 1961), by James S. Albus and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effect of lateral- and longitudinal-range control on allowable entry conditions for a point return from space (National Aeronautics and Space Administration :, 1961), by Alfred G. Boissevain and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Sporadic-E as observed with rockets (National Aeronautics and Space Administration :, 1961), by J. Carl Seddon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental technique for the investigation of tipoff forces associated with stage separation of multistage rocket vehicles (National Aeronautics and Space Administration :, 1962), by Robert L. Gungle, H. Wayne Leonard, William S. Brosier, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the low-subsonic flight characteristics of a model of a reentry vehicle with a thick flat 75 degree swept delta wing and a half-cone fuselage (National Aeronautics and Space Administration :, 1962), by Peter C. Boisseau and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Aerodynamics of Mars entry probe-lander configurations at a Mach number of 10. (National Aeronautics and Space Administration :, 1970), by Robert I. Sammonds, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6646 (National Aeronautics and Space Administration :, 1972), by H. F. Trucks, F. D. Bachtel, J. H. Wise, Uwe Hueter, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On the electron density distribution above the F2 peak (revised) (National Aeronautics and Space Administration :, 1962), by S. J. Bauer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The use of drag modulation to limit the rate at which deceleration increases during nonlifting entry (National Aeronautics and Space Administration :, 1961), by Lional L. Levy and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Velocity requirements for abort from the boost trajectory of a manned lunar mission (National Aeronautics and Space Administration :, 1961), by Robert E. Slye and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Model investigation of the landing characteristics of a reentry spacecraft with a vertical-cylinder air bag for load alleviation (National Aeronautics and Space Administration :, 1962), by John R. McGehee, Victor L. Vaughan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An exploratory investigation of jet-blast effects on a dust-covered surface at low ambient pressure (National Aeronautics and Space Administration :, 1962), by Amos A. Spady and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of the effect of errors in measurement of velocity and flight-path angle on the guidance of a space vehicle approaching the earth (National Aeronautics and Space Administration, 1961), by Jack A. White, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• An analytical method for studying the lateral motion of atmosphere entry vehicles. (National Aeronautics and Space Administration :, 1960), by Robert E. Slye and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6673 (National Aeronautics and Space Administration :, 1972), by George G. Steinmetz, Jag J. Singh, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• On the stability and pointing of an attached double-gimbal experiment package (National Aeronautics and Space Administration, 1972), by Nelson J. Groom, John D. Shaughnessy, Vilas D. Nene, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Centaur space vehicle pressurized propellant feed system tests. (National Aeronautics and Space Administration ;, 1972), by Lewis Research Center (page images at HathiTrust)
• Apollo experience report : flight instrumentation calibration (National Aeronautics and Space Administration ;, 1973), by J. F. DeMoss, United States National Aeronautics and Space Administration, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Sputtering of a vehicle's surface in a space environment / y James R. Redus. (National Aeronautics and Space Administration :, 1962), by Jerome R. Redus and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determining inertias by using the amplitude decay rate of a mechanical oscillating system (National Aeronautics and Space Administration :, 1962), by Gene T. Carpenter, Dan T. Meredith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of phase-change coatings for variable thermal control of spacecraft (National Aeronautics and Space Administration ;, 1972), by Warren C. Kelliher, Philip R. Young, and Langley Research Center (page images at HathiTrust)
• Flight-test results from 2 total temperature probes for air-data measurements up to 2014 ̊K (3625 ̊R) (National Aeronautics and Space Administration :, 1972), by Jack Nugent, Lannie D. Webb, Glenn M. Sakamoto, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A two-impulse plan for performing rendezvous on a once-a-day basis (National Aeronautics and Space Administration :, 1960), by John D. Bird, David F. Thomas, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of solar radiation sheilds for temperature control of space vehicles subjected to large changes in solar energy (National Aeronautics and Space Administration :, 1962), by George J. Nothwang, Frank M. Hamaker, John C. Arvesen, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA Scout ST-1 flight-test results and analyses, launch operations and test vehicle description (National Aeronautics and Space Administration :, 1962), by Robert J. Mayhue and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Feasibility study of a circumlunar photographic experiment (National Aeronautics and Space Administration :, 1962), by William H. Michael, John P. Gapcynski, Robert H. Tolson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Statistical study of effects of insertion errors on ascent trajectories for lunar missions. Harold A. Hamer, Carl R. Huss and John P Mayer. (National Aeronautics and Space Administration :, 1962), by Harold A. Hamer, John P. Mayer, Carl R. Huss, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Optimal filtering and linear prediction applied to a midcourse navigation system for the circumlunar mission (National Aeronautics and Space Administration :, 1962), by John D. McLean, Leonard A. McGee, Stanley F. Schmidt, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The effects of particle size on the optical properties and surface roughness of a glass-balloon-filled black paint (National Aeronautics and Space Administration ;, 1974), by T. M. Heslin, Marvin Harper, James Heaney, and Goddard Space Flight Center (page images at HathiTrust)
• A Simple solar orientation control system for space vehicles. Seymour Salmirs, S. Lawrence Kessler and Otis J. Parker. (National Aeronautics and Space Administration :, 1962), by Seymour Salmirs, Otis J. Parker, S. Lawrence Kessler, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of two thrusting techniques for soft lunar landings starting from a 50-mile altitude circular orbit (National Aeronautics and Space Administration :, 1962), by M. J. Queijo, G. Kimball Miller, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preliminary survey of retrograde velocities required for insertion into low-altitude lunar orbits (National Aeronautics and Space Administration :, 1961), by Morris V. Jenkins, Robert E. Munford, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1823 (National Aeronautics and Space Administration, 1963), by Odell A. Morris, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A real-time space station dynamics and control system simulation. (National Aeronautics and Space Administration :, 1971), by Carolyn Grantham, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• The purposes of environmental testing for scientific satellites (National Aeronautics and Space Administration :, 1961), by John H. Boeckel and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1815 (National Aeronautics and Space Administration, 1963), by Kenneth P. Spreemann, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1820 (National Aeronautics and Space Administration, 1963), by Harold A. Hamer, Ward F. Hodge, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-2561 (National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1965), by Peter L. Raffo, Walter R. Witzke, William D. Klopp, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-3891 (National Aeronautics and Space Administration :, 1967), by Grayson V. Dixon, Jerome Pearson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Trajectory control in rendezvous problems using proportional navigation (National Aeronautics and Space Administration :, 1961), by Luigi S. Cocilani and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of a solar sensor for use in space-vehicle orientation control systems. (National Aeronautics and Space Administration :, 1961), by Paul R. Spencer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Simple formulas for stagnation-point convective heat loads in lunar return. (National Aeronautics and Space Administration :, 1961), by Frederick C. Grant and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of the slosh-damping effectiveness of positive-expulsion bags and diaphragms in spherical tanks (National Aeronautics and Space Administration, 1963), by Andrew J. Stofan and Irving E. Sumner (page images at HathiTrust)
• Rocket measurement of a daytime electron density profile up to 620 kilometers. (National Aeronautics and Space Administration :, 1961), by J. E. Jackson, S. J. Bauer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An investigation of the effects of the time lag due to long transmission distance upon remote control: Phase II - Vehicle experiments, Phase III - Conclusions (National Aeronautics and Space Administration :, 1962), by James L. Adams and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of jet pluming on the static stability of cone-cylinder-flare configurations as a mach number of 9.65 / William F. Hinson and Ralph A. Falanga. (National Aeronautics and Space Administration :, 1962), by William F. Hinson, Ralph A. Falanga, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effectiveness of 3 exit vane cascade configurations for vectoring the thrust of a ducted fan (National Aeronautics and Space Administration :, 1964), by Kenneth W. Mort, Paul F. Yaggy, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• One-dimensional heat conduction through the skin of a vehicle upon entering a planetary atmosphere at constant velocity and entry angle (National Aeronautics and Space Administration :, 1962), by William R. Wells, Charles H. McLellan, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Six-inch subsonic high-temperature arc tunnel for structures and material tests (National Aeronautics and Space Administration, 1963), by Ronald D. Brown, L. Ross Levin, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1624 (National Aeronautics and Space Administration, 1963), by Sandy M. Stubbs, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Absorption and emission characteristics of diffuse spherical enclosures : E.M. Sparrow and V.K. Jonsson. (National Aeronautics and Space Administration :, 1962), by E. M. Sparrow, V. Jonsson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1651 (National Aeronautics and Space Administration, 1963), by Walter A. Reinhardt, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4553 (National Aeronautics and Space Administration ;, 1968), by Vernon Krueger, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4559 (National Aeronautics and Space Administration ;, 1968), by William C. Strack, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Environmental problems of space flight structures I. Ionizing radiation in space and it's influence on spacecraft design (National Aeronautics and Space Administration :, 1962), by Louis F. Vosteen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A preliminary experimental investigation of an energy-absorption process employing frangible metal tubing (National Aeronautics and Space Administration :, 1962), by John R. McGehee and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical investigation of recirculation-pump and radiator-area requirements for flash vaporization in a turboelectric space power system Arthur J. Glassman. (National Aeronautics and Space Administration :, 1962), by Arthur J. Glassman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1663 (National Aeronautics and Space Administration, 1963), by Albert Kaufman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Free-flight measurements of the static and dynamic stability and drag of a 10 degree blunted cone at mach numbers 3.5 and 8.5 Peter F. Intrieri. (National Aeronautics and Space Administration :, 1962), by Peter F. Intrieri and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measured steady-state performance of water vapor jets for use in space vehicle attitude control systems (National Aeronautics and Space Administration :, 1962), by Bruce E. Tinling and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Motions of a short 10 degree blunted cone entering a Martian atmosphere at arbitrary angles of attack and arbitrary pitching rates (National Aeronautics and Space Administration :, 1962), by Victor L. Peterson and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An analytical approach to the design of an automatic discontinuous control system (National Aeronautics and Space Administration :, 1961), by Lawrence W. Taylor, John W. Smith, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Static aerodynamic characteristics of short blunt cones with various nose and base cone angles at Mach numbers from 0.6 to 5.5 and angles of attack to 180 degrees (National Aeronautics and Space Administration :, 1961), by Stuart L. Treon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of the use of a terminal controller technique for reentry guidance of a capsule-type vehicle (National Aeronautics and Space Administration :, 1961), by Edwin C. Foudriat and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measurement of the maximum altitude attained by the X-15 airplane powered with interim rocket engines (National Aeronautics and Space Administration :, 1960), by Wendell H. Stillwell, Terry J. Larson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1864 (National Aeronautics and Space Administration :, 1964), by Thaine W. Reynolds, Edward A. Richley, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Dynamics and column densities of small particles ejected from spacecraft (National Aeronautics and Space Administration ;, 1974), by Robert J. Naumann and George C. Marshall Space Flight Center. Space Sciences Laboratory (page images at HathiTrust)
• Time-dependent polar distribution of outgassing from a spacecraft (National Aeronautics and Space Administration ;, 1974), by John J. Scialdone and Goddard Space Flight Center (page images at HathiTrust)
• Apollo experience report; manned thermal-vacuum testing of spacecraft. (National Aeronautics and Space Administration, 1974), by James C. McLane (page images at HathiTrust)
• NASA TN D-1769 (National Aeronautics and Space Administration, 1963), by Charles E. Duller, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some possibilities for determining the characteristics of the atmospheres of Mars and Venus from gas-dynamic behavior of a probe vehicle (National Aeronautics and Space Administration, 1963), by Alvin Seiff, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A trajectory analysis of a variable-drag payload ejected from a vehicle in a low earth orbit (National Aeronautics and Space Administration :, 1963), by Richard Reid, David B. Middleton, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A Statistical model for synthetic wind profiles for aerospace vehicle design and launching criteria (National Aeronautics and Space Administration, 1963), by Robert M. Henry, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Handling qualities and trajectory requirements for terminal lunar landing, as determined from analog simulation (National Aeronautics and Space Administration :, 1963), by Gene J. Matranga, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Investigation of the landing characteristics of a reentry vehicle having a canted multiple-air-bag load-alleviation system (National Aeronautics and Space Administration :, 1963), by Sandy M. Stubbs, John R. McGehee, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gyroscopic motion of an unsymmetrical satellite under no external forces (National Aeronautics and Space Administration :, 1960), by Manfred E. Kuebler and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Low-speed investigation of cable tension and aerodynamic characteristics of a parawing and spacecraft combination (National Aeronautics and Space Administration :, 1963), by William C. Sleeman and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Surface-temperature distribution on thin-walled bodies subjected to solar radiation in interplanetary space (National Aeronautics and Space Administration :, 1961), by Lester D. Nichols and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of liquid-hydrogen storage problems for unmanned nuclear-powered Mars vehicles (National Aeronautics and Space Administration :, 1962), by R.J. Brun and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Magnetic dipole moment determination by near-field analysis (National Aeronautics and Space Administration ;, 1972), by W. L. Eichhorn and Goddard Space Flight Center (page images at HathiTrust)
• NASA TN D-6342 (National Aeronautics and Space Administration :, 1971), by David R. Brooks (page images at HathiTrust)
• NASA TN D-6397 (National Aeronautics and Space Administration:, 1971), by Robert J. Keynton (page images at HathiTrust)
• Effects of surface contamination on the infrared emissivity and visible-light scattering of highly reflective surfaces at cryogenic temperatures (National Aeronautics and Space Administration, 1971), by Walter Viehmann, Alfred G. Eubanks, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-6590 (National Aeronautics and Space Administration :, 1972), by Bill D. Ingle, John P. Ryan, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Heat pipe investigations (National Aeronautics and Space Administration ;, 1973), by James P. Marshburn and Goddard Space Flight Center (page images at HathiTrust)
• Pressure distribution on two models of a Project Mercury capsule for a mach number range of 1.60 to 6.01 and an angle-of-attack range of 0°degress to 180° (National Aeronautics and Space Administration, 1960), by Robert A. Newlander, E. Brian Pritchard, Nancy L. Taylor, and Langley Research Center (page images at HathiTrust)
• Physical electronics (Lockheed Aircraft Corporation, Lockheed Missiles and Space Division, 1960), by P. M. Fitzgerald (page images at HathiTrust)
• Cluster : inside earth's magnetic shield. (National Aeronautics and Space Administration, 1994), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Space shuttle--returnable, reusable : benefitting life on earth while reducing space costs : looking out for our earth with the space shuttle transportation system (California State Dept. of Commerce, Division of Business and Industry Development, 1973), by California Space Shuttle Task Force and California. Office of Business Development (page images at HathiTrust; US access only)
• Gemini V D4/D7 spectral measurements of space objects and earth-cloud backgrounds (Air Force Cambridge Research Laboratories, Office of Aerospace Research, United States Air Force, 1967), by J. Lovett, R. Nadile, L. Marcotte, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)
• A "worst case" spacecraft environment as observed by SCATHA on 24 April 1979 (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), by E. G. Mullen, Henry B. Garrett, M. S. Gussenhoven, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Spacecraft sheath modification during beam ejection (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1985., 1985), by Shu T. Lai, William J. McNeil, Herbert A. Cohen, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Effects of a time-varying photoelectron flux on spacecraft potential (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1978., 1978), by Henry Berry Garrett and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Charging of spinning spacecraft (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1979., 1979), by Allen G. Rubin, M. F. Tautz, K. H. Bhavnani, and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Ground-based predictors of spacecraft charging during eclipse passage (Hanscom AFB, Massachusetts : Air Force Geophysics Laboratory, Air Force Systems Command, United States Air Force, 1980., 1980), by Arthur H. Wendel and U.S. Air Force Geophysics Laboratory (page images at HathiTrust)
• Physical and mechanical properties of commercial molybdenum-base alloys (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1960., 1960), by J. A. Houck and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• Environmental factors influencing metals applications in space vehicles (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1960., 1960), by J. M. Allen and Defense Metals Information Center (U.S.) (page images at HathiTrust)
• JPL profile (National Aeronautics and Space Administration, 1977), by Jet Propulsion Laboratory (U.S.) and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo Soyuz (National Aeronautics and Space Administration, Office of Public Affairs : for sale by the Supt. of Docs., U.S. Govt. Print. Off, 1976), by Walter Froehlich and United States. National Aeronautics and Space Administration. Office of Public Affairs (page images at HathiTrust)
• Convention on registration of objects launched into outer space : message from the President of the United States transmitting the convention on registration of objects launched into outer space which was signed by the United States at New York on January 24, 1975. (U.S. Govt. Print. Off, 1976), by United States. President (1974-1977 : Ford) (page images at HathiTrust)
• Convention on registration of objects launched into outer space : report from the Committee on Foreign Relations to accompany Ex. G, 94-2. (U.S. Govt. Print. Off., 1976), by United States Senate Committee on Foreign Relations (page images at HathiTrust)
• Space nuclear safety and fuels program : March 1981 (Los Alamos, New Mexico : Los Alamos Scientific Laboratory, 1981., 1981), by S. E. Bronisz, Los Alamos Scientific Laboratory, and United States. Department of Energy (page images at HathiTrust)
• Advanced heat source concepts (Miamisburg, Ohio : Mound Laboratory, 1974., 1974), by J. E. Selle, Monsanto Chemical Company, Mound Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Summary of neutron measurements for the Viking Program (Miamisburg, Ohio : Mound Laboratory, 1975., 1975), by M. E. Anderson, Monsanto Chemical Company, United States. Energy Research and Development Administration, and Mound Laboratory (page images at HathiTrust)
• Potassium superoxide canister evaluation for manned space vehicles (Wright-Patterson Air Force Base, Ohio : Flight Accessories Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by A. W. Optican, United States. Air Force. Systems Command. Aeronautical Systems Division, and North American Aviation (page images at HathiTrust)
• Generation of pulsed, energy-selected metal atom beam by laser vaporization of metal compounds (Hanscom Air Force Base, Massachusetts : Phillips Laboratory, Weapons and Survivability Division, Air Force Systems Command, [1991], 1991), by Terry L. Thiem, Edmond Murad, Richard H. Salter, Rainer A. Dressler, Lyn R. Watson, and USAF Phillips Laboratory. Weapons and Survivability Division (page images at HathiTrust)
• Temperature control systems for space vehicles (Wright-Patterson Air Force Base, Ohio : Directorate of Aeromechanics, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Charles P. Bacha, D. Watanabe, F. I. Honea, United States. Air Force. Systems Command. Aeronautical Systems Division, and North American Aviation. Space and Information Systems Division (page images at HathiTrust)
• Waste collection unit for a space vehicle, MR 1092 (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division,Aerospace Medical Division, Air Research and Development Command, United States Air Force, 1960., 1960), by J. Des Jardins, R. A. Bambenek, J. D. Zeff, United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command, and American Machine and Foundry Company (page images at HathiTrust)
• Measurement of ionic conductivity and temperature in the Apollo 15 plume (L.G. Hanscom Field, Massachusetts : Air Force Cambridge Research Laboratories, Air Force Systems Command, United States Air Force, 1973., 1973), by John L. Heckscher, Robert P. Pagliarulo, and Air Force Cambridge Research Laboratories (U.S.) (page images at HathiTrust)

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