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Propellants

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• Combustion
• Explosives

• Propellants -- Bibliography
• Propellants -- Environmental aspects
• Propellants -- Mathematical models
• Propellants -- Measurement
• Propellants -- Storage
• Propellants -- Technological innovations
• Aerosol propellants
• Gunpowder
• Liquid propellants
• Propellant actuated devices
• Rockets (Aeronautics) -- Fuel
• Solid propellants
• Materials, other; -- Propellants

• Possible implications of the damage by radiation in the storage of propellants in outer space and tentative methods for its measurement (Argonne National Laboratory, 1962), by J. A. McMillan, Argonne National Laboratory, and U.S. Atomic Energy Commission (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)
• Air Force stock fund : hydrazine sales consistent with the Commercial Space Launch Act : report to the Chairman, Committee on Science, Space and Technology, House of Representatives (The Office, 1991), by United States General Accounting Office and Space United States. Congress. House. Committee on Science (page images at HathiTrust)
• Design of coast-phase propellant management system for two-burn Atlas-Centaur flight AC-8 (National Aeronautics and Space Administration ;, 1966), by William A. Groesbeck and Lewis Research Center (page images at HathiTrust)
• Fabrication of an internally insulated filament wound liquid hydrogen propellant tank (National Aeronautics and Space Administration, 1964), by C. B. Shriver, Goodyear Aerospace Corporation, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• 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)
• An experimental investigation of the damping of liquid oscillations in cylindrical tanks with various baffles (National Aeronautics and Space Administration :, 1961), by Milton A. Silveira, H. Wayne Leonard, David G. Stephens, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Reaction of copper and flourine. (National Aeronautics and Space Administration :, 1961), by Patricia M. O'Donnell, Adolph E. Spakowski, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA-AEC liquid-metals corrosion meeting December 7-8, 1960, Washington, D.C. (National Aeronautics and Space Administration :, 1961), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical performance of propellants suitable for electrothermal jet engines (National Aeronautics and Space Administration :, 1961), by John R. Jack and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3749 (National Aeronautics and Space Administration :, 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)
• Ignition of a hydrogen-oxygen rocket engine by addition of fluorine to the oxidant (National Aeronautics and Space Administration :, 1962), by R. James Rollbuhler, David M. Straight, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Liquid-hydrogen-flowmeter calibration facility; preliminary calibrations on some head-type and turbine-type flowmeters (National Aeronautics and Space Administration :, 1961), by Herbert L. Minkin, Howard F. Hobart, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An experimental determination of the dynamic response of a long hydraulic line (National Aeronautics and Space Administration :, 1960), by John D. Regetz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental damping of liquid oscillations in a spherical tank by positive-expulsion bags and diaphragms (National Aeronautics and Space Administration :, 1962), by Andrew J. Stofan, Albert J. Pavli, 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)
• Boiling heat transfer to liquid hydrogen and nitrogen in forced flow (National Aeronautics and Space Administration :, 1962), by James P. Lewis, John F. Kline, Jack H. Goodykoontz, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theory of the fluid oscillations in a circular cylindrical ring tank partially filled with liquid (National Aeronautics and Space Administration :, 1960), by Helmut F. Bauer and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Orbital storage of liquid hydrogen (National Aeronautics and Space Administration :, 1961), by J. R. Olivier, W. E. Dempster, and United States National Aeronautics and Space Administration (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-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-5382 (National Aeronautics and Space Administration ;, 1969), by Richard W. High, Manned Spacecraft Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Determination of local experimental heat-transfer coefficients on combustion side of an ammonia-oxygen rocket (National Aeronautics and Space Administration :, 1961), by Curt H. Liebert and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-7001 (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)
• Lunar storage of liquid propellants / y W. E. Dempster, R. L. Evans and J. R. Olivier. (National Aeronautics and Space Administration :, 1962), by W. E. Dempster, J. R. Olivier, R. L. Evans, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Preliminary study of the effects of ionizing radiations on propellants; the x-irradiation of ammonia and hydrazine (National Aeronautics and Space Administration :, 1962), by Harold W. Lucien and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Experimental study of the effects of weightlessness on the configuration of mercury and alcohol in spherical tanks (National Aeronautics and Space Administration :, 1962), by Donald A. Petrash, Edward W. Otto, Robert F. Zappa, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Simulator for static liquid configuration in propellant tanks subject to reduced gravity (National Aeronautics and Space Administration :, 1966), by William A. Olsen and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of Centaur propellant utilization difference bridge (National Aeronautics and Space Administration, 1967), by O. James Magrini and Lewis Research Center (page images at HathiTrust)
• The electrochemical fluorination of organosilicon compounds (National Aeronautics and Space Administration :, 1961), by Robert E. Seaver and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1831 (National Aeronautics and Space Administration, 1963), by Helmut F. Bauer, George C. Marshall Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• The determination of the helium saturation level of Aerozine-50 and nitrogen tetroxide (National Aeronautics and Space Administration ;, 1971), by Irwin D. Smith, Richard P. Schroats, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Performance of 2 subliming-solid-propellant thrustor systems for attitude control of spacecraft (National Aeronautics and Space Administration :, 1967), by Frank D. Berkopec, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Experimental study of effects of geometric variables on performance of conical rocket - engine exhaust nozzles. (National Aeronautics and Space Administration :, 1961), by Harry E. Bloomer, Pqul E. Renas, Robert J. Antl, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Transfer of cryogenic fluids by an expulsion-bag technique. (National Aeronautics and Space Administration :, 1961), by Paul J. Sirocky 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)
• Static thrust of an annular nozzle with a concave central base (National Aeronautics and Space Administration :, 1960), by Blake W. Corson, Charles E. Mercer, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analytical and experimental investigation of forces and frequencies resulting from liquid sloshing in a spherical tank Andrew J. Stofan and Alfred L. Armstead. (National Aeronautics and Space Administration :, 1962), by Andrew J. Stofan, Alfred L. Armstead, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Thermodynamic consistency of solubility data for the hydrogen-helium vapor-liquid system (National Aeronautics and Space Administration :, 1962), by Irving Brazinsky, Bryon S. Gottfried, 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)
• Experimental determination of spectral and total transmissivities of clouds of small particles (National Aeronautics and Space Administration :, 1962), by Chester D. Lanzo, Robert G. Ragsdale, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Analysis of fluorine gas by reaction with mercury / Robert E. Seaver. (National Aeronautics and Space Administration :, 1962), by Robert E. Seaver 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)
• Ion-thruster propellant utilization (National Aeronautics and Space Administration] ;, 1971), by Harold R. Kaufman, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Properties of some propellant fluids containing hydrogen (Los Alamos Scientific Laboratory of the University of California, 1961), by Don L. Bunker, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Comparison of propellant sloshing parameters obtained from model and full-size Centaur liquid-oxygen tanks (National Aeronautics and Space Administration ;, 1966), by Andrew J. Stofan and Lewis Research Center (page images at HathiTrust)
• QADHD point-kernel radiation shielding computer code to evaluate propellant heating and dose to crew during engine operation (National Aeronautics and Space Administration ;, 1967), by Gerald P. Lahti and Lewis Research Center (page images at HathiTrust)
• Reactor fuse propellants and configurations (Atomic Products Division, 1956), by R. J. Spera, Lamond W. Weiss, S. N. Stilwell, U.S. Atomic Energy Commission, and General Electric Company (page images at HathiTrust)
• Toxicity and other hazards of beryllium and rocket propellants : a literature search (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, [1959], 1959), by William E. Bost and U.S. Atomic Energy Commission (page images at HathiTrust)
• Toxicity and hazards of beryllium and rocket propellants : a literature search (Oak Ridge, Tennessee : United States Atomic Energy Commission, Office of Technical Information, [1960], 1960), by William E. Bost and U.S. Atomic Energy Commission (page images at HathiTrust)
• Production of high speed liquid jets by means of a propellant (Oak Ridge, Tennessee : United States Atomic Energy Commission, Technical Information Service, 1954., 1954), by Brian Dunne, Benedict Cassen, Herbert Gass, Los Angeles University of California, and U.S. Atomic Energy Commission (page images at HathiTrust)
• 2³ factorial in a Latinized rectangular lattice design (Virginia Agricultural Experiment Station, Virginia Polytechnic Institute., 1954), by Boyd Harshbarger (page images at HathiTrust; US access only)
• Carbon dioxide as a propellent for insecticide solutions (U.S. Department of Agriculture, Agricultural Research Administration, Bureau of Entomology and Plant Quarantine, 1948), by Robert A. Fulton and United States. Bureau of Entomology and Plant Quarantine (page images at HathiTrust)
• Propellant-atmosphere system study (Wright-Patterson Air Force Base, Ohio : Wright Air Development Division, Air Research and Development Command, U.S. Air Force, 1961., 1961), by inc. Thompson Ramo Wooldridge, United States. Air Force. Air Research and Development Command, and Wright Air Development Division (page images at HathiTrust)
• 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)
• Proceedings of the High Energy Density Matter (HEDM) contractor's conference held 4-7 June 1995 in Woods Hole MA (Edwards Air Force Base, California : Phillips Laboratory, Propulsion Directorate, Air Force Systems Command, United States Air Force, January 1996., 1996), by Patrick G. Carrick, Simon Tam, and USAF Phillips Laboratory (page images at HathiTrust)
• 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)

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