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Rockets (Aeronautics) -- Fuel

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• Rockets (Aeronautics)
• Propellants
• Fuel

• Rockets (Aeronautics) -- Fuel -- Congresses
• Rockets (Aeronautics) -- Fuel -- Equipment and supplies
• Rockets (Aeronautics) -- Fuel -- Mathematical models
• Rockets (Aeronautics) -- Fuel -- Safety measures
• Rockets (Aeronautics) -- Fuel -- Testing
• Rockets (Aeronautics) -- Fuel -- Thermal properties
• Rockets (Aeronautics) -- Fuel -- Toxicity testing
• Rockets (Aeronautics) -- Fuel -- Toxicology
• Liquid propellants
• Nuclear rockets -- Fuel
• Solid propellants

• Rocket propellants

• Rocket Propellants (New York: Reinhold Pub. Corp.; London: Chapman and Hall, c1958), by Francis A. Warren (page images at HathiTrust)
• Liquid Hydrogen as a Propulsion Fuel, 1945-1959, by John L. Sloop (HTML at NASA)
• Theoretical evaluation of chemical propellants. (Prentice-Hall, 1963), by Roger Lawrence Wilkins (page images at HathiTrust)
• Prediction of explosive yield and other characteristics of liquid propellant rocket explosions : final report, October 13, 1968 (University of Florida, Florida Engineering and Industrial Experiment Station, Dept. of Mechanical Engineering, 1968), by Erich A. Farber, C. F. Bonzon, and F. W. Klement (page images at HathiTrust; US access only)
• Displacement and shattering of propellant droplets; final summary report (Air Force Office of Scientific Research, Combustion Dynamics Division, 1960), by E. Rabin, R. B. Lawhead, A. R. Schallenmuller, and Canoga Park Rocketdyne (page images at HathiTrust)
• Interim report on the thermodynamics of chemical species important to rocket technology.. ([Washington], 1970), by United States. National Bureau of Standards (page images at HathiTrust)
• Handling and use of fluorine and fluorine-oxygen mixtures in rocket systems (Scientific and Technical Information Division, Office of Technology Utilization, National Aeronautics and Space Administration; [for sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1967), by Harold W. Schmidt (page images at HathiTrust)
• Antiproton annihilation propulsion (Air Force Rocket Propulsion Laboratory, Air Force Space Technology Center, Space Division, Air Force Systems Command, 1985), by Robert L Forward, Forward Unlimited, University of Dayton. Research Institute, and Air Force Rocket Propulsion Laboratory (U.S.) (page images at HathiTrust)
• Liquid hydrogen as a propulsion fuel, 1945-1959 (Scientific and Technical Information Office, National Aeronautics and Space Administration, 1978), by John L. Sloop (page images at HathiTrust)
• Compatibility of dispersion strengthened platinum with resistojet propellants (National Aeronautics and Space Administration, Scientific and Technical Information Division ;, 1987), by Margaret V. Whalen, Michael V. Nathal, and Lewis Research Center (page images at HathiTrust)
• Lunar missions using chemical propulsion : system design issues (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1991), by Bryan A. Palaszewski and Lewis Research Center (page images at HathiTrust)
• Effect of throttling on interface behavior and liquid residuals in weightlessness (National Aeronautics and Space Administration ;, 1974), by Eugene P. Symons and Lewis Research Center (page images at HathiTrust)
• Rapid estimation of concentration of aromatic classes in middistillate fuels by high-performance liquid chromatography (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1985), by Dumas A. Otterson, Gary T. Seng, and Lewis Research Center (page images at HathiTrust)
• Thermodynamic analysis of an axial-flow laser-powered thruster (National Aeronautics and Space Administration ;, 1974), by Albert F. Kascak and Lewis Research Center (page images at HathiTrust)
• Performance capability of laser-powered launch vehicles using vertical ascent trajectories (National Aeronautics and Space Administration ;, 1974), by Omer F. Spurlock and Lewis Research Center (page images at HathiTrust)
• Upper stages using liquid propulsion and metallized propellants (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Bryan A. Palaszewski and Lewis Research Center (page images at HathiTrust)
• Modeling of space vehicle propellant mixing (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by John C. Aydelott and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Electrothermal engine propellant storage and feed system study, phase II (National Aeronautics and Space Administration :, 1964), by G. E. Roos, United States National Aeronautics and Space Administration, and Beach Aircraft Corporation (page images at HathiTrust)
• A study of two phase detonation as it relates to rocket motor combustion instability (National Aeronautics and Space Administration ;, 1965), by J. A. Nicholls, Kenneth W. Ragland, Eliahou K. Dabora, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis and test for space shuttle propellant dynamics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), by Robert L. Berry, Leonard J. Demchak, James R. Tegart, Lyndon B. Johnson Space Center, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Martin Marietta Denver Aerospace (page images at HathiTrust)
• Theoretical performance of hydrogen-oxygen rocket thrust chambers (U.S. G.P.O., 1961), by Gilbert K. Sievers, George R. Kinney, and William A. Tomazic (page images at HathiTrust)
• NASA TN D-5845 (National Aeronautics and Space Administration :, 1970), by Carl F. Lorenzo, Eva T. Jun, William G. Costakis, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5331 (National Aeronautics and Space Administration ;, 1969), by Peter G. Batterton, John R. Zeller, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-5699 (National Aeronautics and Space Administration :, 1970), by Walter Brooks Drew, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Compilation of thermodynamic properties, transport properties and theoretical rocket performance of gaseous hydrogen (National Aeronautics and Space Administration, 1960), by Charles R. King and Lewis Research Center (page images at HathiTrust)
• An experimental investigation of two-phase liquid oxygen pumping (National Aeronautics and Space Administration ;, 1973), by Loren A. Gross and George C. Marshall Space Flight Center. Astronautics Laboratory (page images at HathiTrust)
• Measurement of liquid and two-phase hydrogen densities with a capacitance density meter (National Aeronautics and Space Administration ;, 1969), by George E. Turney, Roger W. Snyder, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-4571 (National Aeronautics and Space Administration ;, 1968), by Raymond F. Lacovic, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental performance of a hydrogen-fluorine rocket engine at several chamber pressures and exhaust-nozzle expansion area ratios (National Aeronautics and Space Administration, 1960), by William L. Jones, John W. Gibb, Carl A. Aukerman, and Lewis Research Center (page images at HathiTrust)
• Design and experimental performance of a small centrifugal pump for liquid hydrogen (National Aeronautics and Space Administration, 1960), by George W. Lewis, Melvin J. Hartmann, Edward R. Tysl, and Lewis Research Center (page images at HathiTrust)
• Investigation of injectors for a low-chamber-pressure hydrogen-fluorine rocket engine (National Aeronautics and Space Administration, 1962), by Harold G. Price, Arthur M. Shinn, Robert J. Lubick, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-3716 (National Aeronautics and Space Administration :, 1966), by Henry A. Cole and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-3771 (National Aeronautics and Space Administration ;, 1966), by Richard L. Puthoff, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• A general method for automatic computation of equilibrium compositions and theoretical rocket performance of propellants (National Aeronautics and Space Administration, 1959), by Sanford Gordon, Vearl N. Huff, Frank J. Zeleznik, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-4991 (National Aeronautics and Space Administration :, 1968), by David A. Bittker, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1727 (National Aeronautics and Space Administration, 1963), by Richard L. DeWitt, Harold W. Schmidt, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Technique for predicting high-frequency stability characteristics of gaseous-propellant combustors (National Aeronautics and Space Administration ;, 1973), by Richard J. Priem, Jefferson Y. S. Yang, and Lewis Research Center (page images at HathiTrust)
• FORTRAN IV computer program for calculation of thermodynamic and transport properties of complex chemical systems (National Aeronautics and Space Administration ;, 1973), by Roger A. Svehla, Bonnie J. McBride, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental performance of liquid hydrogen and liquid fluorine in regeneratively cooled rocket engines (National Aeronautics and Space Administration, 1959), by H. W. Douglass, H. G. Price, G. Hennings, and Langley Research Center (page images at HathiTrust)
• Effect of fuel drop size and injector configuration on screaming in a 200-pound-thrust rocket engine using liquid oxygen and heptane (National Advisory Committee for Aeronautics, 1958), by Charles E. Feiler, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (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° (National Advisory Committee for Aeronautics, 1954), by Charles E. Feiler, Gerald Morrell, United States. National Adviosry Committee for Aeronautics, and Lewis Flight Propulsion Laboratory (page images at HathiTrust)
• Theoretical rocket performance of JP-4 fuel with several fluorine-oxygen mixtures assuming frozen composition (National Advisory Committee for Aeronautics, 1957), by Sanford Gordon, Kenneth S. Drellishak, Lewis Flight Propulsion Laboratory, and United States. National Adviosry Committee for Aeronautics (page images at HathiTrust)
• Physical properties and thermodynamic functions of fuels, oxidizers, and products of combustion. (Rand Corp., 1951), by Battelle Memorial Institute. Chemical Research Division (page images at HathiTrust; US access only)
• Theoretical performance of liquid ammonia with liquid oxygen as a rocket propellant (National Advisory Committee for Aeronautics, 1958), by Sanford Gordon and United States National Advisory Committee for Aeronautics (page images at HathiTrust; US access only)
• Research on materials and methods for decontamination of toxic missile propellant spillage (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by J. M. Siegmund, B. T. Poon, R. E. Ogden, R. B. Jackson, United States. Air Force. Systems Command. Aeronautical Systems Division, and Allied Chemical Corporation (page images at HathiTrust)
• Amperometric propellent-component detector (Wright-Patterson Air Force Base, Ohio : Biomedical Laboratory, Aerospace Medical Laboratory, Aeronautical Systems Division, Air Force Systems Command, 1961., 1961), by Nicholas A. Poulos, United States. Air Force. Systems Command. Aeronautical Systems Division, and Olin Mathieson Chemical Corporation (page images at HathiTrust)
• Estimation of performance factors for rocket propellants : a compilation of data from generalized systems and its application to specific propellant combinations (Beacon, N.Y. : Texaco, [1962], 1962), by James Robert Muenger, Leonard Greiner, United States. Air Force. Systems Command. Rocket Research Laboratory, and Inc Texaco (page images at HathiTrust; US access only)
• Calculation of the specific impulse of rocket propellants (Wright-Patterson Air Force Base, Ohio : Headquarters, Air Matériel Command, 1948., 1948), by Rudolph Edse and United States. Army Air Forces. Air Matériel Command (page images at HathiTrust)
• Chemical rocket propulsion. ([U.S. Govt. Print. Off.], 1962), by United States National Aeronautics and Space Administration (page images at HathiTrust)

• 20th meeting bulletin. (Solid Propellant Information Agency, Applied Physics Laboratory, Johns Hopkins University;, 1961), by Riverside Joint Army-Navy-Air Force-ARPA-NASA Panel on Physical Properties of Solid Propellants. 20th meeting (page images at HathiTrust)

• Correlation of local heat-transfer coefficients for single-phase turbulent flow of hydrogen in tubes with temperature ratios to 23 (National Aeronautics and Space Administration ;, 1968), by Maynard F. Taylor and Lewis Research Center (page images at HathiTrust)
• Performance charts for multistage rocket boosters (National Aeronautics and Space Administration, 1961), by John S. MacKay, Richard J. Weber, and Lewis Research Center (page images at HathiTrust)

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