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Space vehicles -- Propulsion systems -- Congresses

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• Space vehicles -- Propulsion systems
• Space vehicles -- Congresses

• Proceedings. (U. S. Govt. Print. Off., 1960), by Boston Symposium on Advanced Propulsion Concepts. 2d, Avco-Everett Research Laboratory, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Proceedings of the Sixth AFOSR Symposium on Advanced Propulsion Concepts, v. 1. (Air Force Office of Scientific Research; [for sale by the Supt. of Docs., U.S. Govt. Print. Off., Washington], 1972), by N.Y.) AFOSR Symposium on Advanced Propulsion Concepts. (6th : 1971 : Niagara Falls, Bell Aerospace Company, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Power for spacecraft. (National Aeronautics and Space Administration, Office of Scientific and Technical Information; [for sale by the Superintendent of Documents, U. S. Govt. Print. Off.], 1963), by Ill.) NASA-University Conference on the Science and Technology of Space Exploration (1962 : Chicago (page images at HathiTrust)
• Radiation energy conversion in space : technical papers prepared for the third NASA Conference on Radiation Energy Conversion at NASA Ames Research Center, Moffett Field, California, January 26-28, 1978 (American Institute of Aeronautics and Astronautics, 1978), by NASA Conference on Radiation Energy Conversion (3rd : 1978 : Ames Research Center), Kenneth W. Billman, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Space Transportation Propulsion Technology Symposium (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by Space Transportation Propulsion Technology Symposium (1990 : Pennsylvania State University), Pennsylvania State University, and United States. Office of Space Flight (page images at HathiTrust)
• Propulsion systems lubricants (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), by Tex.) Air Force-Navy-Industry Propulsion Systems Lubricants Conference (1960 : San Antonio, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and Southwest Research Institute (page images at HathiTrust)

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

• Reusable Launch Vehicle: Technology Development and Test Program (1995), by National Research Council Aeronautics and Space Engineering Board (page images with commentary at NAP)
• Propulsion systems for space flight. (McGraw-Hill, 1960), by William R. Corliss (page images at HathiTrust)
• Proceedings. (Air Force Office of Scientific Research, 1957), by AFOSR Symposium on Advanced Propulsion Concepts and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Si può già tentare un viaggio dalla terra alla luna? : relazione di esperienze eseguite coi propulsori a doppia reazione ; altre esperienze, Nuovo processo per la stereoscopia diretta ; Bombe da fucile ; L'automobile ippico nello sport (Società editrice libraria, 1923), by Luigi Gussalli (page images at HathiTrust; US access only)
• Glossary of terms and table of conversion factors used in design of chemical propulsion systems. (National Aeronautics and Space Administration, 1975), by United States National Aeronautics and Space Administration (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)
• Ion propulsion for spacecraft. (National Aeronautics and Space Administration, Lewis Research Center, 1977), by Lewis Research Center (page images at HathiTrust)
• Fusion energy for space missions in the 21st century : executive summary (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Norman R. Schulze and United States. National Aeronautics and Space Administration. Office of Safety and Mission Quality. Technical Standards Division (page images at HathiTrust)
• Fusion energy for space missions in the 21st century (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991), by Norman R. Schulze and United States. National Aeronautics and Space Administration. Office of Safety and Mission Quality. Technical Standards Division (page images at HathiTrust)
• Electric arc discharge damage to ion thruster grids (National Aeronautics and Space Administration ;, 1974), by Dale D. Beebe, Robert C. Finke, Shigeo Nakanishi, and Lewis Research Center (page images at HathiTrust)
• Effect of type of load on stress analysis of thin-walled ducts (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by J. B. Min, P. K. Aggarwal, and George C. Marshall Space Flight Center (page images at HathiTrust)
• High-performance auxiliary-propulsion ion thruster with ion-machined accelerator grid (National Aeronautics and Space Administration ;, 1975), by Wayne R. Hudson, Bruce A. Banks, and Lewis Research Center (page images at HathiTrust)
• Comparison of thermal analytic model with experimental test results for 30-centimeter-diameter engineering model mercury ion thruster (National Aeronautics and Space Administration ;, 1977), by Jon C. Oglebay and United States National Aeronautics and Space Administration (page images at HathiTrust)
• An evaluation of composite propulsion for single-stage-to-orbit vehicles designed for horizontal take-off (National Aeronautics and Space Administration ;, 1977), by J. A. Martin and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Purging of a tank-mounted multilayer insulation system by gas diffusion (National Aeronautics and Space Administration, Scientific Information Office ;, 1978), by Irving E. Sumner and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Operating characteristics of a hollow-cathode neutralizer for 5- and 8-centimeter-diameter electron-bombardment mercury ion thrusters (National Aeronautics and Space Administration ;, 1975), by Albert J. Weigand and Lewis Research Center (page images at HathiTrust)
• Accelerated life test of sputtering and anode deposit spalling in a small mercury ion thruster (National Aeronautics and Space Administration ;, 1975), by John L. Power and Lewis Research Center (page images at HathiTrust)
• Concept for a power system controller for large space electrical power systems (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by Louis F. Lollar, James R. Graves, John R. Lanier, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Feasibility study of LITVC for Shuttle SRB (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), by C. L. Martin, L. B. Powers, George C. Marshall Space Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A study of personnel propulsion devices for use in the vicinty of the moon (National Aeronautics and Space Administration;, 1966), by N. Economou, Langley Research Center, and Bell Aerospace Corporation. Bell Aerosystems Company (page images at HathiTrust)
• Vaporization in liquid uranium bearing systems ... (National Aeronautics and Space Administration, 1965), by Larry Kaufman, Maynard F. Taylor, Edward T. Peters, Inc ManLabs, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Technology requirements for advanced earth-orbital transportation systems, duel-mode propulsion (National Aeronautics and Space Administration ;, 1977), by Rudolph C. Haefeli, Martin Marietta Corporation, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Theoretical calculations of radiant heat transfer properties of particle-seeded gases (National Aeronautics and Space Administration ;, 1970), by J. Richard Williams, J. D. Clement, A. S. Shenoy, Lewis Research Center, and Georgia Institute of Technology (page images at HathiTrust)
• Orbital transfer vehicle engine technology : baffled injector design, fabrication and verification (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program ;, 1991), by J. A. Schneider, Lewis Research Center, and GenCorp. Aerojet Propulsion Division (page images at HathiTrust)
• NASA TN D-2080 (National Aeronautics and Space Administration, 1963), by Ernie W. Spisz, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Estimation of critical temperature for surface ion currents from electron emission data (National Aeronautics and Space Administration :, 1962), by Thaine W. Reynolds and United States National Aeronautics and Space Administration (page images at HathiTrust)
• 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)
• Low-density foam for insulating liquid-hydrogen tanks (National Aeronautics and Space Administration ;, 1969), by Irving E. Sumner, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• Emission spectra from high-pressure hydrogen-oxygen combustion (National Aeronautics and Space Administration :, 1962), by Marshall C. Burrows, Louis A. Povinelli, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effects of simulated retrorockets on the aerodynamic characteristics of a body of revolution at Mach numbers from 0.25 to 1.90 (National Aeronautics and Space Administration :, 1962), by Victor L. Peterson, Robert L. McKenzie, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-4054 (National Aeronautics and Space Administration ;, 1967), by Eugene V. Pawlik, Paul D. Reader, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design and performance of a liquid-hydrogen, liquid-oxygen gas generator for driving a 1000-horsepower turbine (National Aeronautics and Space Administration :, 1962), by Nick J. Sekas, Loren W. Acker, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Performance of several cast nickel-base alloys as turbojet-engine bucket materials at 1650° F (National Aeronautics and Space Administration :, 1962), by James R. Johnston, John H. Sinclair, Charles A. Gyorgak, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Modulated entry (National Aeronautics and Space Administration :, 1960), by Frederick C. Grant and Langley Research Center (page images at HathiTrust)
• NASA TN D-5844 (National Aeronautics and Space Administration :, 1970), by David C. Byers, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Optimal three-dimensional resusable tug trajectories for planetary missions including correction for nodal precession (National Aeronautics and Space Administration ;, 1976), by Janos Borsody and Lewis Research Center (page images at HathiTrust)
• Purging of multilayer insulation by gas diffusion (U.S. National Aeronautics and Space Administration ;, 1976), by Irving E. Sumner, Charles M. Spuckler, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust)
• A graphical method for estimating ion-rocket performance (National Aeronautics and Space Administration :, 1960), by Thaine W. Reynolds, J. Howard Childs, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-5993 (National Aeronautics and Space Administration :, 1971), by Mark H. Waters and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-5996 (National Aeronautics and Space Administration :, 1970), by William C. Strack, Frank J. Hrack, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• One thousand hour endurance test of a glass-coated accelerator grid on a 15-centimeter-diameter kaufman thruster (National Aeronautics and Space Administration :, 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)
• 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-5692 (National Aeronautics and Space Administration ;, 1970), by Terrill W. Putnam, Ronald H. Smith, Flight Research Center (U.S.), and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Satellite and space propulsion systems (National Aeronautics and Space Administration, 1960), by Wolfgang E. Moeckel (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)
• An experimental evaluation of metallic diaphragms for positive fuel expulsion in the Atmosphere Explorer hydrazine propulsion subsystem (National Aeronautics and Space Administration ;, 1973), by William L. Woodruff and Goddard Space Flight Center (page images at HathiTrust)
• Apollo experience report : descent propulsion system (National Aeronautics and Space Administration ;, 1973), by William R. Hammock, Arlie E. Fisher, Eldon C. Currie, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Test results from a breadboard cryogenic propellant conditioning assembly (National Aeronautics and Space Administration ;, 1974), by Henry P. Stinson and George C. Marshall Space Flight Center. Astronautics Laboratory (page images at HathiTrust)
• NASA TN D-3210 (National Aeronautics and Space Administration :, 1966), by Irving E. Sumner, United States National Aeronautics and Space Administration, and Lewis Research Center (page images at HathiTrust; US access only)
• 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)
• Basic performance of a multilayer insulation system containing 20 to 160 layers (National Aeronautics and Space Administration ;, 1974), by Robert J. Stochl and Lewis Research Center (page images at HathiTrust)
• NASA TN D-1876 (National Aeronautics and Space Administration, 1963), by William Lewis, Robert G. Dorsch, Robert J. Blade, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Apollo experience report : ascent propulsion system (National Aeronautics and Space Administration ;, 1973), by Clarence E. Humphries, Reuben E. Taylor, and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Apollo experience report : launch escape propulsion subsystem (National Aeronautics and Space Administration ;, 1973), by Neil A. Townsend and Manned Spacecraft Center (U.S.) (page images at HathiTrust)
• Analytic and experimental evaluation of shadow shields and their support members for thermal control of space vehicles (National Aeronautics and Space Administration ;, 1974), by Robert J. Boyle, Robert J. Stochl, and Lewis Research Center (page images at HathiTrust)
• NASA TN D-1710 (National Aeronautics and Space Administration, 1963), by Arthur J. Glassman, Samuel M. Futral, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• NASA TN D-1664 (National Aeronautics and Space Administration, 1963), by David P. Harry, Lewis Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-1650 (National Aeronautics and Space Administration, 1963), by David H. Hickey, Leo P. Hall, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Measured steady-state performance of water vapor jets for use in space vehicle attitude control systems (National Aeronautics and Space Administration :, 1962), by Bruce E. Tinling and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Numerical solution of two-dimensional Possion equation : Theory and application to electrostatic-ion-engine analysis (National Aeronautics and Space Administration :, 1962), by Vladimir Hamza, Edward A. Richley, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• NASA TN D-3489 (National Aeronautics and Space Administration :, 1966), by Dale W. Harris, J. J. Ketchman, R. J. Burian, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Apollo experience report : service propulsion subsytem (National Aeronautics and Space Administration ;, 1973), by Cecil R. Gibson, James A. Wood, and Lyndon B. Johnson Space Center (page images at HathiTrust)
• Computer programs for pressurization (ramp) and pressurized expulsion from a cryogenic liquid propellant tank (National Aeronautics and Space Administration ;, 1974), by Philip A. Masters and Lewis Research Center (page images at HathiTrust)
• Rotating fluidized bed reactor for space nuclear propulsion : annual report: design studies and experimental results (Brookhaven National Laboratory, in the 20th century), by Brookhaven National Laboratory. Dept. of Applied Science. Engineering Division, U.S. Atomic Energy Commission, United States National Aeronautics and Space Administration, and United States. Space Nuclear Systems Office (page images at HathiTrust)
• Plasma propulsion studies : summer, 1959 (Los Alamos Scientific Laboratory of the University of California, 1960), by M. E. Ebel, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Single stage orbiting vehicles (Los Alamos Scientific Laboratory of the University of California, 1962), by Ralph S. Cooper, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Performance of optimized multistage rockets (Los Alamos Scientific Laboratory of the University of California, 1962), by Ralph S. Cooper, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Fast reactor rocket engines--criticality (Los Alamos Scientific Laboratory of the University of California, 1962), by Ralph S. Cooper, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• A Monte Carlo calculation of neutron heating in a nuclear rocket propellant tank (Los Alamos Scientific Laboratory of the University of California, 1963), by J. R. Streetman, G. A. Graves, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Mission analysis for nuclear propulsion (Los Alamos Scientific Laboratory of the University of California, 1961), by Ralph S. Cooper, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• Nuclear powered lunar rockets (Los Alamos Scientific Laboratory of the University of California, 1960), by Ralph S. Cooper, U.S. Atomic Energy Commission, and Los Alamos Scientific Laboratory (page images at HathiTrust)
• A preliminary report on nuclear rocket dynamics and control (Los Alamos Scientific Laboratory of the University of California, 1961), by Ronald R. Mohler, E. A. Wheatley, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Kiwi-B system dynamics (Los Alamos Scientific Laboratory of the University of California, 1961), by E. A. Wheatley, B. G. Strait, O. A. Farmer, Ronald R. Mohler, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• Solution of a problem to obtain the optimum energy for a rocket initially in a circular orbit (Los Alamos Scientific Laboratory of the University of California, 1960), by George A. Baker, John G. Wills, Los Alamos Scientific Laboratory, and U.S. Atomic Energy Commission (page images at HathiTrust)
• SNAP I radioisotope-fueled turboelectric power conversion system summary : January 1957 to June 1959 (United States. Dept. of Energy ;, 1960), by Paul J. Dick, Martin Company. Nuclear Division, United States. Department of Energy. Office of Scientific and Technical Information, U.S. Atomic Energy Commission. Division of Technical Information, and United States. Department of Energy (page images at HathiTrust)
• Engines for interstellar ships (Translation Division, Foreign Technology Division, 1963), by R. G. Perelʹman (page images at HathiTrust; US access only)
• Propulsion for deep space (Cleveland, 1966), by Lewis Research Center. Electromagnetic Propulsion Division (page images at HathiTrust)
• Studies of design criteria for welded structures subjected to a biaxial stress field (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processess, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by Bruce L. Baird and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Potential capabilities of the Stirling engine for space power (Wright-Patterson Air Force Base, Ohio : Directorate of Aeromechanics, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), by General Motors Corporation. Allison Division and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)

More items available under broader and related terms at left.