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Rocket engines

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• Rockets (Aeronautics)

• Rockets (Aeronautics)

• Rocket engines -- Combustion
• Rocket engines -- Control systems
• Electric rocket engines
• Liquid propellant rocket engines
• Nuclear rocket engines
• Solid propellant rocket engines

• Rocket motors
• Rockets (Aeronautics) -- Motors

• How to Design, Build and Test Small Liquid-Fuel Rocket Engines, by Leroy J. Krzycki (illustrated HTML at gramlich.net)
• Some observations of base heating at Mach 3.0 on a simulated missile with JP-4 liquid-oxygen rocket / (Washington, D.C. : National Aeronautics and Space Administration, 1960), by Nick E. Samanich, Donald D. Barnett, J. Calvin Lovell, and Lewis Research Center (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)
• Organizational maintenance manual (including repair parts and special tools lists) : 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)
• Organizational maintenance manual (including repair parts and special tools lists) : 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, [1992]), by United States. Department of the Army (page images at HathiTrust)
• Air admixture to exhaust jets / (Washington, D.C. : NACA, 1953), by Eugen Sänger and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• National altitude rocket test facilities / (Washington, D.C. : National Aeronautics and Space Administration ; Washington, D.C. : For sale by the Office of Technical Services, Department of Commerce [distributor], 1964), by J. A. Suddreth (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)
• Numerical procedures for calculating real fluid properties of normal and parahydrogen / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Fredric N. Goldberg, Angela M. Haferd, and Lewis Research Center (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)
• Effect of propellant-feed-system coupling and hydraulic parameters on analysis of chugging / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Don J. Wood, Robert G. Dorsch, and Lewis Research Center (page images at HathiTrust)
• Studies of the exhaust products from solid propellant rocket motors / (Arnold Air Force Station, Tenn. : Von Kármán Gas Dynamics Facility, Arnold Engineering Development Center, Air Force Systems Command, [1976]), by R Dawbarn, Max Kinslow, United States National Aeronautics and Space Administration, and Arnold Engineering Development Center (page images at HathiTrust)
• Thermal stratification potential in rocket engine coolant channels / ([Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Kenneth J. Kacynski and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program (page images at HathiTrust)
• Program user's manual for optimizing the design of a liquid or gaseous propellant rocket engine with the automated combustor design code AUTOCOM / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by R. H. Reichel, Lewis Research Center, and Aerophysics Research Corporation (page images at HathiTrust)
• Experimental determination of potential lunar surface organic contamination in the lunar module descent-engine exhaust / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by D. A. Flory and Manned Spacecraft Center (U.S.) (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)
• Static thrust augmentation of a rocket-ejector system with a heated supersonic primary jet / (Washington, [D.C.] : National Aeronautics and Space Administration, 1962), by Albert J. Simonson, James W. Schmeer, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Experimental evaluation of high-purity-silica reinforced ablative composites as nozzle sections of 7.8-inch-(19.8 CM) diameter throat storable-propellant rocket engine / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Donald A. Peterson and Lewis Research Center (page images at HathiTrust)
• A resonance-tube igniter for hydrogen-oxygen rocket engines / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by E. William Conrad, Albert J. Pavli, and Lewis Research Center (page images at HathiTrust)
• Experimental and analytical study of one- and two-component flows in spherical chambers / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Bruce V. Johnson, Lewis Research Center, and United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Nondestructive testing of Scout rocket motors / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1972), by Arthur E. Oaks, Langley Research Center, and General Electric Company (page images at HathiTrust)
• Simulator tests to study hot-flow problems related to a gas core reactor / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1973), by John W. Poole, Lewis Research Center, and Humphreys Corporation (page images at HathiTrust)
• Propellant vaporization as a design criterion for rocket-engine combustion chambers / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1960), by Richard J. Priem, Marcus F. Heidmann, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Perigee propulsion for orbital launch of nuclear rockets / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1962), by Paul G. Johnson, Frank E. Rom, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Reliability and effective thermal conductivity of three metallic-ceramic composite insulating coatings on cooled hydrogen-oxygen rockets / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Harold G. Price, Richard J. Quentmeyer, Ralph L. Schacht, and Lewis Research Center (page images at HathiTrust)
• Evaluation of a thin-film, heat-flux probe for measuring gas velocities in an unstable rocket combustor / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1967), by Frederick P. Povinelli, Robert D. Ingebo, and Lewis Research Center (page images at HathiTrust)
• Seeded gas thrusters and related system components / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by John W. Poole, Merle L. Thorpe, Lewis Research Center, and Humphreys Corporation (page images at HathiTrust)
• Design and evaluation of an oxidant-fuel-ratio-zoned rocket injector for high performance and ablative engine compatibility / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Jerry M. Winter, Arthur M. Shinn, Albert J. Pavli, and Lewis Research Center (page images at HathiTrust)
• Experimental evaluation of a tuned electromagnetic damper for vibration control of cryogenic turbopump rotors / (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 Eliseo DiRusso, Gerald V. Brown, and Lewis Research Center (page images at HathiTrust)
• Loads analysis and testing of flight configuration solid rocket motor outer boot ring segments / (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 Rafiq Ahmed and George C. Marshall Space Flight Center. Structures and Dynamics Laboratory (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)
• NASA/MSFC multilayer diffusion models and computer programs; version 5 / (Washington : National Aeronautics and Space Administration ;, 1975), by R. K. Dumbauld, J. R. Bjorklund, and H.E. Cramer Company (page images at HathiTrust)
• Coolant-side heat-transfer rates for a hydrogen-oxygen rocket and a new technique for data correlation / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by Ralph L. Schacht, Richard J. Quentmeyer, and Lewis Research Center (page images at HathiTrust)
• Apollo experience report : thermal protection from engine-plume environments / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by J. Thomas Taylor and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Analytical study of moderator wall cooling of gaseous nuclear rocket engines / ([Washington] : National Aeronautics and Space Administration, [1965]), by G. H. McLafferty, United Aircraft Corporation, and United States National Aeronautics and Space Administration (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)
• Frequency response of a vaporization process to distorted acoustic disturbances (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Marcus F. Heidmann, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Comparison of vibrations of a combination of solid-rocket launch vehicle and payload during a ground firing and launching / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by James A. Schoenster, Harold B. Pierce, and Langley Research Center (page images at HathiTrust)
• Upper-stage space-shuttle propulsion by means of separate scramjet and rocket engines / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Leo C. Franciscus, John L. Allen, and Lewis Research Center (page images at HathiTrust)
• Technology test bed : the future for rocket engine design. ([United States] : Office of Space Flight, 1991), by United States. Office of Space Flight (page images at HathiTrust)
• Advanced earth-to-orbit propulsion technology 1994 : proceedings of a conference held at NASA George C. Marshall Space Flight Center, Marshall Space Flight Center, May 17-19, 1994 / (Huntsville, Ala. : National Aeronautics and Space Administration, Marshall Space Flight Center, 1994), by Ala) Advanced Earth-to-Orbit Propulsion Technology (6th : 1994 : Huntsville, S. T. Wu, R. J. Richmond, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Combustor performance with various hydrogen-oxygen injection methods in a 200-pound-thrust rocket engine / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by Marcus F. Heidmann, Louis Baker, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Distribution of neutral propellant from electric thrusters onto spacecraft components / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969]), by Thaine W. Reynolds, Edward A. Richley, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Characteristics of the optical radiation from Kaufman thrusters / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Nelson L. Milder, James S. Sovey, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Liquid rocket actuators and operators (Washington] National Aeronautics and Space Administration, 1973), by James G Absalom and United States National Aeronautics and Space Administration (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)
• Liquid rocket engine combustion stabilization devices / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the National Technical Information Service, 1974), by Russell B. Keller, L. P. Combs, and Howard W. Douglass (page images at HathiTrust)
• Captive-fired testing of solid rocket motors (Washington] National Aeronautics and Space Administration, 1971), by James W Kordig and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Base heating investigations on a 1/10 scale model Centaur stage using short-duration high altitude testing techniques. Contract no. NAS 3-3227. (Buffalo, Cornell Aeronautical Laboratory, Inc., 1963), by C. L. Matthis (page images at HathiTrust)
• An Investigation of instabilities characteristic of liquid propellant rocket motors : (Inyokern, China Lake, Calif. : U.S. Naval Ordnance Test Station, 1952), by Saul Pollock and Calif.) Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• Effect of blade leading edge thickness on cavitation performance of 80.6 ̊helical inducer in hydrogen / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1970), by Royce D. Moore, Phillip R. Meng, 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)
• Annular slit colloid thruster research and development / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Kenneth W. Stark, William A. Burton, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Use of high-conductivity cladding material on D-shaped coolant passages in nozzles to reduce tube-wall crest temperatures / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Ronald G. Huff, Frank B. Molls, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analytic performance of two-grid accelerator designs for Kaufman thrusters / (Washington, D.C.: National Aeronautics and Space Administration:, 1971), by Walter C. Lathem (page images at HathiTrust; US access only)
• Performance of two subliming-solid-propellant thrustor systems for attitude control of spacecraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1967), by Frank D. Berkopec, Lewis 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)
• Thirteenth Workshop for Computational Fluid Dyanmic Applications in Rocket Propulsion and Launch Vehicle Technology : proceedings of a workshop held at Huntsville, Alabama, April 25-27, 1995 /, by Ala.) Workshop for Computational Fluid Dynamic Applications in Rocket Propulsion and Launch Vehicle Technology (13th : 1995 : Huntsville, R. W. Williams, and George C. Marshall Space Flight Center (page images at HathiTrust; US access only)
• Liquid rocket engine turbopump shafts and couplings / (Washington] : National Aeronautics and Space Administration, 1972), by L. K. Severud and C. C. Purdy (page images at HathiTrust; US access only)
• Flow field resulting from forward-facing nozzles exhausting near a large cylindrical body at free-stream Mach numbers of 3.0, 4.5, and 6.0 / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by James A. Martin, Robert J. McGhee, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Comparative in-flight thrust measurements of the SERT II ion thruster, (Washington, National Aeronautics and Space Administration; [for sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Va.], 1970), by William C. Nieberding, Frank D. Berkopec, and Daniel J. Lesco (page images at HathiTrust; US access only)
• A method for computing extremal maximum-range thrust-limited rocket trajectories with application to lunar transport / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1970), by A. Gary Childs, Athena T. Markos, Ernest S. Armstrong, Langley 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)
• Evaluation of tangential velocity effects on spinning transverse combustion instability / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1966), by Marcus F. Heidmann, Charles E. Feiler, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Resonance tube ignition of hydrogen-oxygen mixtures / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1971), by Bert R. Phillips, Albert J. Pavli, 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)
• Design and development of a micropound extended range thrust stand (MERTS) / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1971), by Kenneth W. Stark, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Fabrication of welded rocket motor cases; a committee report. (New York, American Welding Society, c1961), by American Welding Society. Missiles and Rockets Welded Fabrication Committee (page images at HathiTrust; US access only)
• Liquid rocket engine turbopump rotating-shaft seals / ([Washington, D.C.] : National Aeronautics and Space Administration, 1978), by R. E. Burcham and Russell B. Keller (page images at HathiTrust)
• Liquid propellant rocket combustion instability. (Washington : Scientific and Technical Information Office, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1972), by David T. Harrje and Frederick H. Reardon (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)
• Space shuttle : follow-up evaluation of NASA's solid rocket motor procurement : report to the chairman, Committee on Government Operations, House of Representatives / (Washington, D.C. : The Office, [1989]), by United States General Accounting Office and United States House Committee on Government Operations (page images at HathiTrust)
• Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Janos Borsody, Fred Teren, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental verification of a double dead-time model describing chugging in liquid bipropellant rocket engines / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by John R. Szuch, Leon M. Wenzel, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Space shuttle main engine high pressure fuel pump aft platform seal cavity flow analysis / (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 S. A. Lowry, L. W. Keeton, and George C. Marshall Space Flight Center (page images at HathiTrust)
• High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion / ([Washington, DC] : National Aeronautics and Space Administration, Scientific and Technical Information Division ; [Springfield, Va. : For sale by the National Technical Information Service], 1988), by Philip A. Masters, Harold G. Price, Elizabeth S. Armstrong, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division (page images at HathiTrust)
• Computer code for single-point thermodynamic analysis of hydrogen/oxygen expander-cycle rocket engines / (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 Arthur J. Glassman, Scott M. Jones, and Lewis Research Center (page images at HathiTrust)
• Some injector element detail effects on screech in hydrogen-oxygen rockets / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Ned P. Hannum and Lewis Research Center (page images at HathiTrust)
• Plasma tests of sprayed coatings for rocket thrust chambers / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Arthur N. Curren, Walter K. Love, and Lewis Research Center (page images at HathiTrust)
• Some aspects of FLOX-methane rocket engine throttling / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by D. E. Sokolowski, Edwin J. Seigwarth, Ned P. Hannum, and Lewis Research Center (page images at HathiTrust)
• Fabrication of liquid-rocket thrust chambers by electroforming / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1974), by Rudolph A. Duscha, John M. Kazaroff, and Lewis Research Center (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)
• Instrumentation of sampling aircraft for measurement of launch vehicle effluents / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Dewey E. Wornom, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Research in the use of electrets in measuring effluents from rocket exhaust of the Space Shuttle (6.4 percent scaled model) and Viking I launch / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Michael Susko and George C. Marshall Space Flight Center (page images at HathiTrust)
• Ice nucleus activity measurements of solid rocket motor exhaust particles / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1986), by Vernon W. Keller and George C. Marshall Space Flight Center (page images at HathiTrust)
• Identification and management of filament-wound case stiffness parameters / (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 V. Verderaime, M. Rheinfurth, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and George C. Marshall Space Flight Center (page images at HathiTrust)
• SBASI : actuated pyrotechnic time delay initiator / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by S. J. Salter, G. L. McDougal, R. E. Lundberg, Langley Research Center, and MB Associates (page images at HathiTrust)
• Demonstration of a sterilizable solid rocket motor system / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by E. J. Mastrolia, W. L. Lambert, G. M. Santerre, Langley Research Center, and Aerojet Solid Propulsion Company (page images at HathiTrust)
• Solid Rocket Motor Witness Test / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ; Springfield, Va. : For sale by the National Technical Information Service, 1991), by Christopher S. Welch, College of William and Mary. Dept. of Physics, and Langley Research Center (page images at HathiTrust)
• Analysis of the measured effects of the principal exhaust effluents from solid rocket motors / (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 R. Dawbarn, D. J. Watson, Max Kinslow, Arnold Engineering Development Center, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• A technique for thrust-vector orientation during manual control of lunar landings from a synchronous orbit / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by L. Keith Barker, M. J. Queijo, and Langley Research Center (page images at HathiTrust)
• Performance evaluation of fixed- and variable-area rocket exhaust diffusers using single and clustered nozzles with and without gimbaling / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Bruce E. Church, Richard J. Quentmeyer, William L. Jones, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Modulated entry / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)
• A describing-function analysis of the stability of a launch vehicle with nonlinear thrust vectoring / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1965]), by Harold C. Lester and Langley Research Center (page images at HathiTrust)
• Application of various techniques for determining local heat-transfer coefficients in a rocket engine from transient experimental data / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Curt H. Liebert, Ronald W. Grant, James E. Hatch, and Lewis Research Center (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)
• Experimental investigation in an altitude test facility of burning of excess combustibles in a rocket engine exhaust / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Harry E. Bloomer, Robert J. Antl, Paul E. Renas, and Lewis Research Center (page images at HathiTrust)
• Analysis of one-dimensional ion rocket with grid neutralization / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Harold Mirels, Burt M. Rosenbaum, 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, [1966]), by Richard J. Roelke, David G. Evans, Roy G. Stabe, and Lewis Research 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)
• Heat treatment for improved stress-corrosion resistance of 17-7 ph stainless steel / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Carl R. Johnson, John D. Grimsley, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Comparison of predicted and experimental cavitation performance of 84 ̊helical inducer in water and hydrogen / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1970]), by George Kovich and Lewis Research Center (page images at HathiTrust)
• A preliminary investigation of the destruction of solid-propellant rocket motors by impact from small particles / (Washington : National Aeronautics and Space Administration, [1960]), by David J. Carter and Langley Research Center (page images at HathiTrust)
• Liquid behavior in the reservoir of the sound suppressor system / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Helmut F. Bauer and George C. Marshall Space Flight Center (page images at HathiTrust)
• Displacement of disintegrated liquid jets in crossflow / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Frederick P. Povinelli and Lewis Research Center (page images at HathiTrust)
• Experimental heat-transfer study of a regeneratively cooled hydrogen-fluorine rocket engine at low chamber pressure / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Arthur N. Curren 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)
• Propulsion fundamentals / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by James F. Connors and Lewis Research Center (page images at HathiTrust)
• Calculation of rocket vertical-flight performance / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by John C. Evvard 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)
• Evaluation of speech suppression concepts in a 20 000 pound thrust hydrogen oxygen rocket / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by John P. Wanhainen, Louis M. Russell, Ned P. Hannum, and Lewis Research Center (page images at HathiTrust)
• Launch deflector design criteria and their application to the Saturn C-1 deflector. : R.L. Evans and O.L. Sparks. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1963]), by R. L. Evans, O. L. Sparks, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Far-field noise characteristics of Saturn static tests / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1961]), by Wade D. Dorland and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance analysis of high-energy chemical stages for interplanetary missions / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Walter H. Stafford, Carmen R. Catalfamo, Sam H. Harlin, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Free jet impingement normal to a curved surface in a vacuum / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Leonard V. Clark, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Gaseous-hydrogen-liquid-oxygen rocket combustion at supercritical chamber pressures / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1967]), by Martin Hersch, Edward J. Rice, and Lewis Research Center (page images at HathiTrust)
• An explicit solution for the lagrange mulipliers on the sincular subarc of an optimal trajectory / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Rowland E. Burns and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental performance of an ion rocket engine using a rectangular-slab porous-tungsten emitter / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, 1962]), by Ronald J. Cybulski, David L. Lockwood, Joseph T. Kotnik, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A manual abort guidance technique with concentric-flight-plan rendezvous / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by G. Kimball Miller, L. Keith Barker, Langley Research Center, 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)
• Loads induced on a flat plate at a Mach number of 4.5 with a sonic or supersonic jet exhausting normal to the surface / (Washington : National Aeronautics and Space Administration, [1963]), by William Letko and Langley Research Center (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)
• Investigation of a 4.0-inch-mean-diameter four-stage reentry turbine for auxiliary power drives / (Washington, [D.C.] : National Aeronautics and Space Administration, 1960), by Robert Y. Wong, Monroe Daniel E., David L. Darmstadt, Langley 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)
• Experimental investigation of base heating and rocket hinge moments for a simulated missile through a Mach number range of 0.8 to 2.0 / (Washington D.C. : National Aeronautics and Space Administration, 1959), by Bruce G. Chiccine, Arthur M. Shinn, Alfred S. Valerino, and Langley Research Center (page images at HathiTrust)
• 6670-newton attitude-control thruster using hydrogen-oxygen propellant / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by National Technical Information Service, 1977), by Larry H. Gordon and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thermodynamic and chemical paramters of the exhaust effluents from the HARPOON booster motor / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by J. Briscoe Stephens, Arnold I. Goldford, inc Science Applications, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Effect of low-stiffness closeout overwrap on rocket thrust-chamber life / (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 Harold J. Kasper, J. Joseph Notardonato, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Measurements of the extinction parameters of hot seeded hydrogen at high pressures / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Tecchnical Information Service, 1971]), by J. Richard Williams, J. D. Clement, W. L. Partain, Lewis Research Center, and Georgia Institute of Technology (page images at HathiTrust)
• Development and demonstration of flueric sounding rocket motor ignition / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1974]), by Vincent P. Marchese, Langley Research Center, and Singer Company. Kearfott Division (page images at HathiTrust)
• Acoustic efficiency trends for high thrust boosters / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by S. H. Guest and George C. Marshall Space Flight Center (page images at HathiTrust)
• Effect of ambient air velocity on atomization of two impinging water jets / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by David A. Bittker and Lewis Research Center (page images at HathiTrust)
• Sounding rocket reliability reassessment / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Abrom Hisler and Goddard Space Flight Center (page images at HathiTrust)
• A modern transistorized instrumentation system for acoustical data acquisition / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1964]), by Wade D. Dorland, Denis Ulderic Noiseux, C. C. Thornton, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Analysis of the transient radiation heat transfer of an uncooled rocket engine operating outside Earth's atmosphere / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by William H. Robbins and Lewis Research Center (page images at HathiTrust)
• Analysis of effects of rocket-engine design parameters on regenerative-cooling capabilities of several propellants / (Washington : National Aeronautics and Space Administration, [1959]), by Arthur N. Curren, Howard W. Douglass, Harold G. Price, and Lewis Research Center (page images at HathiTrust)
• Optimal finite-thrust transfer between planet-approach and departure asymptotes with specified intermediate orbit / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by Edward A. Willis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Wing-on and wing-off longitudinal characteristics of an airplane configuration having a thin unswept wing of aspect ratio 3, as obtained from rocket-propelled models at Mach numbers from 0.8 to 1.4 / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Clarence L. Gillis, A. James Vitale, and Langley Research Center (page images at HathiTrust)
• On the design of acoustic liners for rocket engines : Helmholtz resonators evaluated with a rocket combustor / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969), by Bert Phillips, Louis M. Russell, Ned P. Hannum, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Characterization of pressure perturbations induced in a rocket combustor by a machine gun / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1969), by D. E. Sokolowski, E. William Conrad, David W. Vincent, 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)
• M-1 engine subscale injector tests / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Herbert E. Scott, Ali H. Mansour, Harry E. Bloomer, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of rocket-powered ejectors for pumping liquid oxygen and liquid hydrogen / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Leo C. Franciscus, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Minimum thrust for correcting Keplerian orbits with application to interplanetary guidance / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1968]), by Frederick W. Boltz, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Vibration characteristics of 1/8-scale dynamic models of the space-shuttle solid-rocket boosters / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Sumner A. Leadbetter, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Liquid-phase heat-release rates of the systems hydrazine-nitric acid and unsymmetrical dimethylhydrazine-nitric acid / (Washington : National Aeronautics and Space Administration, [1960]), by Dezso Somogyi, Charles E. Feiler, and Lewis Research Center (page images at HathiTrust)
• Effect of propellant and catalyst bed temperatures on thrust buildup in several hydrogen peroxide reaction control rockets / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce, [1960]), by John P. Wanhainen, Richard L. DeWitt, Phil S. Ross, and Lewis Research Center (page images at HathiTrust)
• Measured effects of gaseous flow system dynamics on acoustic-mode combustion instability / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by John F. Groeneweg, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Performance of various oxide-magazine cathodes in Kaufman thrusters / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by David C. Byers and Lewis Research Center (page images at HathiTrust)
• Thermometric determination of oxidant-fuel distribution within a rocket combustor / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by Marshall C. Burrows, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Effect of injection element radial distribution and chamber geometry on acoustic-mode instability in a hydrogen oxygen rocket / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by John P. Wanhainen, C. Joe Morgan, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Experimental determination of equivalent solid bodies to represent jets exhausting into a Mach 2.20 external stream / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1969), by Lawrence E. Putnam, Francis J. Capone, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Solid-propellant combustion instability and the role of velocity coupling / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Louis A. Povinelli, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Simplified analytical model for use in design of pump-inlet accumulators for the prevention of liquid-rocket longitudinal oscillation (POGO) (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1969), by William Lewis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Back flow from jet plumes in vacuum / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Norman T. Grier, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Torque and leakage rates of various lubricated lip seal designs at a peripheral velocity of 120 feet per second / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1969]), by Lawrence P. Ludwig, Robert L. Johnson, Thomas N. Strom, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Interim summary of liquid rocket acoustic-mode-instability studies at a nominal thrust of 20,000 pounds / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by E. William Conrad, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thrust measurements of a hollow-cathode discharge / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Aaron Snyder, Bruce A. Banks, Lewis Research Center, and United States National Aeronautics and Space Administration (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)
• Cyclic furnace oxidation of clad WI-52 systems and 1040 ̊and 1090 ̊C (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1972), by Michael A. Gedwill, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental investigation of jet impingement on surfaces of fine particles in a vacuum environment / (Washington, D.C. : National Aeronautics and Space Administration : For sale by the Office of Technical Services, Dept. of Commerce, [1965]), by Norman S. Land, Leonard V. Clark, and Langley Research Center (page images at HathiTrust)
• A high-performance 250-pound-thrust rocket engine utilizing coaxial-flow injection of JP-4 fuel and liquid oxygen / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Samuel Stein and Langley Research Center (page images at HathiTrust)
• Control of combustion-chamber pressure and oxidant-fuel ratio for a regeneratively cooled hydrogen-fluorine rocket engine / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by Edward W. Otto, Richard A. Flage, and Lewis Research Center (page images at HathiTrust)
• Analytical comparison of hydrazine with primary propellants as the turbine drive fluid for hydrogen-fluorine and hydrogen-oxygen altitude stage rockets / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by William T. Wintucky and Lewis Research Center (page images at HathiTrust)
• Vaporization rates of ethanol sprays in a combustor with low-frequency fluctuations of combustion-gas pressure / Robert D. Ingebo. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Robert D. Ingebo and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Some numerical comparisons of three-body trajectories with patched two-body trajectories for low thrust rockets / (Washington, D. C. : National Aeronautics and Space Administration ; Springfield, Va. : for sale by the Clearinghouse for Federal Scientific and Technical Information, 1968), by William C. Strack, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of differential absorption lidar technique for measurements of anhydrous hydrogen chloride from solid rocket motors using a deuterium fluoride laser / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Clayton H. Bair, Frank Allario, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Contamination of spacecraft surfaces dowmstream of a Kaufman thruster / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1971]), by Thaine W. Reynolds, Edward A. Richley, and Lewis Research Center (page images at HathiTrust)
• A manual method for control of the thrust axis during planar ascent from the lunar surface to a circular orbit / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia], 1966), by Herman S. Fletcher, L. Keith Barker, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analysis of frequency response characteristics of propellant vaporization / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1966), by Marcus F. Heidmann, Paul R. Wieber, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• YLR99-RM-1 rocket engine operating experience in the X-15 aircraft / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1964), by James F. Maher, Vincent N. Capasso, C. Wayne Ottinger, Flight Research Center (U.S.), 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)
• Effect of thrust per element on combustion stability characteristics of hydrogen-oxygen rocket engines / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1968), by Reino J. Salmi, Ned P. Hannum, John P. Wanhainen, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Analysis of chugging in liquid-bipropellant rocket engines using propellants with different vaporization rates / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 22151], 1965), by Leon M. Wenzel, John R. Szuch, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Noise reduction shape factors in the low-frequency range / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by J. Ronald Bailey and Franklin D. Hart (page images at HathiTrust; US access only)
• Experimental study of multi-component coaxial-flow jets in short chambers / (Washington, D.C. : National Aeronautics and Space Administration, 1968), by Bruce V. Johnson (page images at HathiTrust; US access only)
• Development of launch vehicle malfunction effects model / (Washington, D.C. : National Aeronautics and Space Administration, 1965), by inc Sperry Gyroscope Company (page images at HathiTrust; US access only)
• Effect of turbulent mixing on average fuel temperatures in a gas-core nuclear rocket engine / (Washington, D.C. : National Aeronautics and Space Administration ; [For sale by the Clearinghouse for Federal Scientific and Technical Information, Springfield, Virginia 2215], 1968), by Albert F. Kascak, Annie J. Easley, Lewis Research Center, 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)
• A study of refractory materials for seal and bearing applications in aircraft accessory units and rocket motors /, by L. B. Sibley, W. H. Goldthwaite, C. L. Peterson, W. J. Zielenbach, C. M. Allen, United States. Air Force. Air Research and Development Command. sponsor, Wright Air Development Center issuing body, and Battelle Memorial Institute (page images at HathiTrust)
• An experimental investigation of the effect of high-pressure tailpipe length on the performance of solid-propellant motors for rocket-powered aircraft / (Washington, D.C. : National Advisory Committee for Aeronautics, 1952), by Charles J. Rodriguez, 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)
• Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by Vearl N. Huff, Sanford Gordon, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Starting of rocket engine at conditions of simulated altitude using crude monoethylaniline and other fuels with mixed acid / (Washington, D.C. : National Advisory Committee for Aeronautics, [1950]), by Gerald Morrell, Jack C. Humphrey, John L. Sloop, Dezso J. Ladanyi, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Theoretical performance of liquid ammonia, hydrazine and mixture of liquid ammonia and hydrazine as fuels with liquid oxygen bifluoride as oxidant for rocket engines (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by Vearl N. Huff, Sanford Gordon, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Theoretical performance of diborane as a rocket fuel / (Washington, D.C. : National Advisory Committee for Aeronautics, [1949]), by Vearl N. Huff, Virginia C. Erdmann, Clyde S. Calvert, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and OH) Lewis Flight Propulsion Laboratory (Cleveland (page images at HathiTrust)
• Chemical and physical factors affecting combustion in fuel : nitric acid systems / (Washington, D.C. : National Advisory Committee for Aeronautics, 1958), by James Baker, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (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)
• Design and evaluation of a turbojet-exhaust simulator with a solid-propellant rocket motor for free-flight research / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Abraham Leiss, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Analytical and experimental studies of spherical solid-propellant rocket motors / (Washington, D.C. : National Advisory Committee for Aeronautics, 1957), by Joseph G. Thibodaux, George Wright, Robert L. Swain, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• New developments in welded fabrication of large solid-fuel rocket-motor cases /, by M. D. Randall, D. C. Martin, R. E. Monroe, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• An evaluation of materials for rocket-motor cases based on minimum weight concepts /, by W. P. Achbach, R. J. Runck, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• Hydrogen-oxygen chemical reaction kinetics in rocket engine combustion / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, VA : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1967), by Martin Hersch, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Proceedings of the Air Force-Navy-Industry Propulsion Systems Lubricants Conference, November 15, 16, 17, 1960 /, by Tex.) Air Force-Navy-Industry Propulsion Systems Lubricants Conference (1960 : San Antonio, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States. sponsor, and sponsor Southwest Research Institute (page images at HathiTrust)
• On the application of air-coupled seismic waves /, by Francis A. Crowley, Henry A. Ossing, and Air Force Cambridge Research Laboratories (U.S.) (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)
• 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)
• Effects of thruster firings on the shuttle environment 1 : neutral gas composition /, by Donald Edward Hunton and sponsor U.S. Air Force Geophysics Laboratory. Ionospheric Physics Division (page images at HathiTrust)
• An approximate analysis of the shock structure in underexpanded plumes /, by C. E. Peters, W. J. Phares, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Jet simulation techniques : simulation of temperature effects by altering gas composition /, by W. L. Peters, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Exhaust plume thermodynamic effects on nonaxisymmetric nozzle afterbody performance in transonic flow /, by C. E. Robinson, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• An evaluation of jet simulation parameters for nozzle afterbody testing at transonic Mach numbers /, by William Lee Peters, United States. Air Force. Systems Command. issuing body, sponsor Arnold Engineering Development Center, and Inc. ARO (page images at HathiTrust)
• Computation of axisymmetric separated nozzle-afterbody flow /, by James L. Jacocks, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Evaluation of various exhaust nozzles at free-stream Mach numbers from 0.6 to. 3.0 /, by Lawrence L. Galigher, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• Wind tunnel testing of interactions of high altitude rocket plumes with the free stream /, by H. K. Smithson, D. L. Whitfield, L. L. Price, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Exhaust plume temperature effects on nozzle afterbody performance over the transonic Mach number range /, by C. E. Robinson, M. Dean High, Inc. ARO, Arnold Engineering Development Center. sponsor, and United States. Air Force. Systems Command. issuing body (page images at HathiTrust)
• Evaluation of boattail geometry and exhaust plume temperature effects on nozzle afterbody drag at transonic Mach numbers /, by L. L. Galigher, R. C. Bauer, Steven F. Yaros, Arnold Engineering Development Center. sponsor, United States. Air Force. Systems Command. issuing body, and Inc. ARO (page images at HathiTrust)
• A two-fluid model for missile exhaust trail expansion /, by Christopher Sherman, Arnold W. Guess, issuing body Air Force Cambridge Research Laboratories (U.S.), and sponsor GCA Corporation (page images at HathiTrust)
• Experimental studies on the interaction of strong sound fields with free convection boundary layers /, by E. E. Soehngen, J. P. Holman, and issuing body Aerospace Research Laboratories (U.S.) (page images at HathiTrust)
• Temperatures in structures., by L. C. Barrett, Charles J. Thorne, H. J. Fletcher, United States. Navy Department. Bureau of Ordnance. sponsor, and Calif.). issuing body Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• Temperatures in structures., by Charles J. Thorne, United States. Navy Department. Bureau of Ordnance. sponsor, and Calif.). issuing body Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• Temperatures in structures., by Charles J. Thorne, United States. Navy Department. Bureau of Ordnance. sponsor, and Calif.). issuing body Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• Temperatures in structures., by Otto Neall Strand, Charles J. Thorne, United States. Navy Department. Bureau of Ordnance. sponsor, and Calif.). issuing body Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• Temperatures in structures., by Raymond E. Smithson, United States. Navy Department. Bureau of Ordnance. sponsor, and Calif.). issuing body Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• Temperatures in structures., by Charles J. Thorne, United States. Navy Department. Bureau of Ordnance. sponsor, and Calif.). issuing body Naval Ordnance Test Station (China Lake (page images at HathiTrust)
• 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)
• Experimental and analytical study of rolling-velocity amplification during the thrusting process for two 10-inch-diameter spherical rocket motors in free flight / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by C. William Martz, Robert L. Swain, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)

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