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Space vehicles -- Materials -- Testing

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• Space vehicles -- Materials
• Space vehicles -- Testing
• Materials -- Testing

• Space vehicles -- Materials -- Testing -- Statistics
• Space vehicles -- Materials -- Testing -- Tables
• Space stations -- Materials -- Testing
• Space vehicles -- Materials -- Environmental testing
• Space vehicles -- Materials -- Fire testing
• Space vehicles -- Materials -- Impact testing
• Space vehicles -- Auxiliary power supply -- Materials -- Testing
• Space vehicles -- Control rockets -- Materials -- Testing
• Space vehicles -- Heating and ventilation -- Control -- Materials -- Testing
• Space vehicles -- Lubrication -- Materials -- Testing
• Space vehicles -- Materials -- Magnetic properties -- Testing
• Space vehicles -- Meteoroid protection -- Materials -- Testing
• Space vehicles -- Nuclear power plants -- Materials -- Testing
• Space vehicles -- Optical equipment -- Materials -- Testing
• Space vehicles -- Propulsion systems -- Materials -- Testing
• Space vehicles -- Shielding (Radiation) -- Materials -- Testing

• Thermal and structural tests of René 41 honeycomb integral-tank concept for future space transportation systems (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by John L. Shideler and Dryden Flight Research Facility (page images at HathiTrust)
• Spacecraft under random loading (National Aeronautics and Space Administration, 1964), by Joshua E. Greenspon, J.C. Engineering Research Associates, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Development of elastomeric thermal shield materials (National Aeronautics and Space Administration, 1965), by C. M. Dolan, General Electric Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Space radiation resistant transparent polymeric materials (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), by C. Giori, T. Yamauchi, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• The effect of resin composition and fillers on the performance of a molded charring ablator (National Aeronautics and Space Administration, 1963), by Roger W. Peters, Kenneth L. Wadlin, and Langley Research Center (page images at HathiTrust)
• The effect of ring distortions on buckling of blunt conical shells (National Aeronautics and Space Administration ;, 1975), by Walter L. Heard, Wendell B. Stephens, Melvin S. Anderson, and Langley Research Center (page images at HathiTrust)
• NASA TN D-2165 (National Aeronautics and Space Administration :, 1964), by Marvin B. Dow, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Effect of weight, density, and heat load on thermal shielding performance of phenolic nylon (National Aeronautics and Space Administration :, 1964), by Andrew J. Chapman and Langley Research Center (page images at HathiTrust)
• An experimental investigation of the impact resistance of double-sheet structures at velocities to 24,000 feet per second (National Aeronautics and Space Administration ;, 1962), by C. Robert Nysmith, James L. Summers, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A preliminary experimental investigation of an energy-absorption process employing frangible metal tubing (National Aeronautics and Space Administration :, 1962), by John R. McGehee and United States National Aeronautics and Space Administration (page images at HathiTrust)
• In-flight and laboratory vacuum-friction test results (National Aeronautics and Space Administration ;, 1973), by E. J. Devine, William A. Leasure, Harold E. Evans, and Goddard Space Flight Center (page images at HathiTrust)
• Study of hypervelocity micro-particle cratering (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1960., 1960), by Richards L. G., L. S. Holloway, U.S. Atomic Energy Commission, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
• Hypervelocity micro-particle impact on thin foils (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1961., 1961), by Richards L. G., J. W. Jr Gehring, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)

• A compilation of outgassing data for spacecraft materials (National Aeronautics and Space Administration ;, 1973), by William A. Campbell, John J. Park, Richard S. Marriott, and Goddard Space Flight Center (page images at HathiTrust)

• Outgassing data for spacecraft materials (National Aeronautics and Space Administration ;, 1975), by William A. Campbell, John J. Park, Richard S. Marriott, and Goddard Space Flight Center (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)

• Environmental testing of contaminant producing materials from the integrated life support system (N.A.S.A., 1967), by William S. Hodgkiss, James S. Swinehart, and Richard H. Johns (page images at HathiTrust; US access only)
• Irradiation effects of 22 and 240 Mev protons on several transistors and solar cells (National Aeronautics and Space Administration, 1961), by William C. Hulten, John L. Patterson, William C. Honaker, and Langley Research Center (page images at HathiTrust)
• Environmental test contribution to spacecraft reliability (National Aeronautics and Space Administration ;, 1967), by Kenneth R. Mercy and Goddard Space Flight Center (page images at HathiTrust)
• NASA TN D-1716 (National Aeronautics and Space Administration, 1963), by W. B. Fussell, J. H. Henninger, J. J. Triolo, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Toxic hazards research unit : annual technical report : 1968 (Wright-Patterson Air Force Base, Ohio : Aerospace Medical Research Laboratory, Aerospace Medical Division, Air Force Systems Command, United States Air Force, 1968., 1968), by J. D. MacEwen, E. H. Vernot, and Aerospace Medical Research Laboratory (U.S.) (page images at HathiTrust)

• Third LDEF post-retrieval symposium (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995), by Va.) Post-Retrieval Symposium (3rd : 1993 : Williamsburg, Arlene S Levine, Langeley Research Center, American Institute of Aeronautics and Astronautics, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Experimental study of transient effects in dielectric materials caused by electron irradiation (National Aeronautics and Space Administration ;, 1965), by George M. Storti, Clifford S. Frank, Donald H. Phillips, and Langley Research Center (page images at HathiTrust)
• Experimental study of transmission and backscatter of 0.075 to 1.0 MeV electrons by aluminum and stainless steel (National Aeronautics and Space Administration ;, 1968), by William E. Miller, Herbert D. Hendricks, and Langley Research Center (page images at HathiTrust)

• Effects of shunt capacitance on transient effects caused by electron irradiation of a polyethylene terephthalate insulated ribbon wire (National Aeronautics and Space Administration ;, 1966), by William E. Miller, Donald H. Phillips, and Langley Research Center (page images at HathiTrust)

• Reduced-pressure environment effects on rolling-element fatigue life with super-refined mineral oil lubricant (National Aeronautics and Space Administration ;, 1968), by David W. Reichard, Erwin V. Zaretsky, Richard J. Parker, and Lewis Research Center (page images at HathiTrust)

• Ultrahigh-vacuum creep behavior of columbium and tantalum alloys at 2000 ̊and 2200 ̊F for times greater than 1000 hours (National Aeronautics and Space Administration ;, 1966), by Robert H. Titran, Robert W. Hall, and Lewis Research Center (page images at HathiTrust)

• Fused fluoride coatings as solid lubricants in liquid sodium, hydrogen, vacuum, and air (National Aeronautics and Space Administration :, 1964), by Harold E. Sliney, Gordon P. Allen, Thomas N. Strom, and Lewis Research Center (page images at HathiTrust)

• Apollo command module mockup flammability tests (National Aeronautics and Space Administration ;, 1970), by Richard W. Bricker and Manned Spacecraft Center (U.S.) (page images at HathiTrust)

• Explorer 16 (National Aeronautics and Space Administration :, 1964), by United States National Aeronautics and Space Administration (page images at HathiTrust)
• The Explorer XVI micrometeoroid satellite. Preliminary results for the period December 16, 1962 through January 13, 1963 (National Aeronautics and Space Administration, 1963), by Earl C. Hastings and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Mass transfer in a 1370 ̊C (2500 ̊F) lithium thermal-convection loop (National Aeronautics and Space Administration ;, 1974), by Coulson M. Scheuermann and Lewis Research Center (page images at HathiTrust)
• Electrical heating tests of uranium dioxide external fuel configuration at emitter temperature of 1900 K (National Aeronautics and Space Administration ;, 1974), by Dominic C. DiIanni, John T. Mayer, and Lewis Research Center (page images at HathiTrust)
• System reliability analysis through corona testing (National Aeronautics and Space Administration ;, 1975), by Vincent R. Lalli, Ernest A. Koutnik, Lawrence A. Mueller, and Lewis Research Center (page images at HathiTrust)
• Development of a cobalt-tungsten ferromagnetic, high-temperature, structural alloy (National Aeronautics and Space Administration ;, 1968), by Richard L. Ashbrook and Lewis Research Center (page images at HathiTrust)
• Compatibility tests of materials for a lithium-cooled space power reactor concept (National Aeronautics and Space Administration ;, 1973), by John H. Sinclair and Lewis Research Center (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)

• Achievement of a low-outgassing white paint system for spacecraft thermal control (National Aeronautics and Space Administration ;, 1972), by Benjamin Seidenberg, Carroll H. Clatterbuck, John J. Park, and Goddard Space Flight Center (page images at HathiTrust)

• Friction, wear, and decomposition mechanisms for various polymer compositions in vacuum to 10⁻⁹ millimeter of mercury (National Aeronautics and Space Administration, 1963), by Donald H. Buckley, Robert L. Johnson, and Lewis Research Center (page images at HathiTrust)
• Adaptation of an MoS₂ "in situ" process for lubricating spacecraft mechanical components (National Aeronautics and Space Administration :, 1964), by Charles E. Vest and Goddard Space Flight Center (page images at HathiTrust)

• Bumper-protected laminated spacecraft mainwalls (National Aeronautics and Space Administration ;, 1971), by Ray Kinslow, Langley Research Center, and Tennessee Technological University (page images at HathiTrust)
• NASA TR R-279 (National Aeronautics and Space Administration ;, 1968), by Robert G. Thomson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• An investigation of high-velocity impact cratering into nonmetallic targets and correlation of penetration data for metallic and nonmetallic targets (National Aeronautics and Space Administration, 1961), by William H. Kinard, Rufus Davis Collins, and Langley Research Center (page images at HathiTrust)
• NASA TN D-1784 (National Aeronautics and Space Administration ;, 1963), by Donald H. Humes, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)

• Materials technology for an advanced space power nuclear reactor concept : program summary (National Aeronautics and Space Administration ;, 1975), by Richard E. Gluyas, Gordon K. Watson, and Lewis Research Center (page images at HathiTrust)
• Evaluation of refractory-metal-clad uranium nitride and uranium dioxide fuel pins after irradiation for times up to 10,450 hours at 990 ̊C (National Aeronautics and Space Administration ;, 1975), by Kenneth J. Bowles, Richard E. Gluyas, and Lewis Research Center (page images at HathiTrust)

• Effects of 1.2 and 0.30 Mev electrons on the optical transmission properties of several transparent materials (National Aeronautics and Space Administration :, 1965), by Gilbert A. Haynes, William E. Miller, and Langley Research Center (page images at HathiTrust)

• Hydrogen environment embrittlement of Astroloy and Udimet 700 (nickel-base) and V-57 (iron-base) superalloys (National Aeronautics and Space Administration ;, 1975), by Hugh R. Gray, Joseph P. Joyce, and Lewis Research Center (page images at HathiTrust)
• Conventionally cast and forged copper alloy for high-heat-flux thrust chambers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1987), by John M. Kazaroff, George A. Repas, and Lewis Research Center (page images at HathiTrust)

• Effects of simulated space environment on Skylab parasol material (National Aeronautics and Space Administration ;, 1974), by Wayne S. Slemp and Langley Research Center (page images at HathiTrust)

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