displaying 91 - 100 results in total 156
Pope, R. B.; Riccitiello, S. R.; Parker, J. A.
view article (1.0)Evaluation of a Polyurethane Foam for Ablative Protection at Low Heating Rates.National Aeronautics and Space Administration, Ames Research Center, Moffett Field, CAJournal of Spacecraft and Rockets, Vol. 6, No. 1, 74-76, January 1969Radnofsky, M. I.
view article (1.0)History and Development of Nonflammable Material for Apollo Spacecraft.National Aeronautics and Space Administration, Manned Spacecraft Center, Houston, TXAerospace Medicine, Vol. 40, No. 11, 1181-1185, November 1969Botteri, B. P.; Manheim, J.
view article (1.0)Fire and Explosion Suppression Techniques.National Aeronautics and Space Administration, Manned Spacecraft Center, Houston, TXAerospace Medicine, Vol. 40, No. 11, 1186-1193, November 1969Friedman, R.; Sacksteder, K. R.; Urban, D.
view article (1.0)Risks, Designs, and Research for Fire Safety in Spacecraft. NASA Technical Memorandum.NASA Lewis Research Center, Cleveland, OH; Sverdrup Technology, Inc., Brook Park, OH['NASA TM 105317', 'E-6672', 'WU-323-53-62']National Aeronautics and Space Administration, Washington, DC, NASA TM 105317; E-6672; WU-323-53-62
1991
20 p.National Fire Protection Association. Fall Meeting. November 19, 1991, Quebec, Canada, 1991Hill, K.; Hornstein, B.
view article (1.0)Detection of Hydrogen-Air Fires and Explosions in Aerospace Vehicles Via OH Band and Water Band Emission. Technical Documentary Report. June 1, 1962-November 30, 1962.Air Force Materials Lab., Wright-Patterson AFB, OH['ASD-TDR-63-113', 'Project 6075', 'Task No. 607501']ASD-TDR-63-113; Project 6075; Task No. 607501
April 1963
103 p.Pippen, D. L.; Stradling, J. S.
view article (1.0)Techniques for Determination of Flash and Fire Points and Impact Sensitivity of Materials in a Gaseous Oxygen Environment.National Aeronautics and Space Administration, Las Cruces, NMMaterials Research and Standards, Vol. 11, No. 6, 35-53, June 1971Jamison, H. H.
view article (1.0)Development of a Gaseous Oxygen Impact Testing Method.National Aeronautics and Space Administration, Las Cruces, NMMaterials Research and Standards, Vol. 11, No. 6, 22-27, June 1971Nguyen, B. K.; Pham, B. T.
view article (1.0)Assessing LOX Compatibility for Aluminum-Lithium Alloys.Air Force System Command, Edwards AFB, CAASTM STP 1111ASTM STP 1111American Society for Testing and Materials. Flammability and Sensitivity of Materials in Oxygen-Enriched Atmospheres. Volume 5. Symposium Sponsored by ASTM Committee G-4 on Compatibility and Sensitivity of Materials in Oxygen Enriched Atmospheres. ASTM STP 1111. May 14-16, 1991, ASTM, Philadelphia, PA, Cocoa Beach, FL, Stoltzfus, J. M.; McIlroy, K., Editors, 463-474 p., 1991Knight, W. H.; Hitchens, A. L.; Ewbank, N. M.; Gigas, G.
view article (1.0)Nondestructive Testing of Apollo CSM Spacecraft Ordnance Devices by Neutron Radiography.North American Rockwell Corp., Downey, CA; North American Rockwell Corp., Canoga Park, CAFranklin Institute of the State of Pennsylvania. Electroexplosive Devices, 6th Symposium. July 8-10, 1969, San Francisco, CA, 2-11.1/16 p., 1969Staklis, A. A.
view article (1.0)Fire Control for Spacecraft With 5-psia Oxygen Atmospheres.National Aeronautics and Space Administration, Houston, TXMSC Technical Note S-136MSC Technical Note S-136
1967
79 p.