High temperature polyimide materials in extreme temperature environments

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Johnson, Theodore F ^a,b   Gates, Thomas S ^a,c  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b Metals and Thermal Structures Branch   (United States)

^c Mechanics and Durability Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTER SOFTWARE REUSABILITY; DURABILITY; HIGH TEMPERATURE EFFECTS; NASA; PHYSICAL PROPERTIES; POLYMERS; RESEARCH AIRCRAFT; REUSABLE ROCKETS; SOFTWARE TESTING; VEHICLES;

CRYOGENIC TEMPERATURES; HIGH SPEED CIVIL TRANSPORTS; HIGH TEMPERATURE MATERIALS; MECHANICAL AND PHYSICAL PROPERTIES; NASA LANGLEY RESEARCH CENTER; OPERATING TEMPERATURE; POLYMERIC COMPOSITE MATERIALS; REUSABLE LAUNCH VEHICLES;

C (PROGRAMMING LANGUAGE);

EID: 85063551582     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1214     Document Type: Conference Paper

References (10)

1. Cook, S., "The X-33 Advanced Technology Demonstrator," Presented at the American Institute of Aeronautics and Astronautics (AIAA) Dynamics Specialists Conference, AIAA-96-1195, April 1996.
2. NASA, "Access to Space Study Final Report," NASA Headquarters, Washington DC, July 1993.
3. th Congress of the International Astronautical Federation (IAF), IAF 94-V3.534, October 1994.
4. Johnson, T. F., Natividad, R., Rivers, H. K., Smith, R., "Thermal Structures Technology Development for Reusable Launch Vehicle Cryogenic Propellant Tanks," Presented at the Space Technologies and Application International Forum, Albuquerque; NM, January 1998.
5. Myers, D. E., Martin, C. J., Blosser, M. L., "Parametric Weight Comparison of Advanced Metallic, Ceramic Tile, and Ceramic Blanket Thermal Protection Systems (TPS)," NASA Technical Memorandum L-17651, August 1997.
6. Weiser, E. S., Johnson, T. F., St. Clair, T. L., Echigo, Y., Kaneshiro, H., Grimsley, B.W., "Polyimide Foams for Aerospace Vehicles", Journal of High Performance Polyimides, Volume 12 (2000), pp. 1-12.
7. Committee on High Speed Research, National Research Council, "U.S. Supersonic Commercial Aircraft - Assessing NASA's High Speed Research Program," National Academy Press, Washington, D.C., 1997.
8. Robinson, M. J., "Composite Cryogenic Propellant Tank Development," Proceedings of the 35th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, HiltonHead, SC, 18-21 April 1994.
9. NASA Handbook 8060.1C (NHB 8060.1C), "Flammability, Odor, Offgassing, and Compatibility Requirements and Test Procedures for Material in Environments that Support Combustion," April 1991.
10. Robinson, M. J., Stoltzfus, J.M., Owens, T. N., "Composite Material Compatibility with Liquid Oxygen", 38th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, Kissimmee, FL, 7-10 April 1997.