Thermal response of integral multicomponent composite thermal protection systems
Author:
Affiliation:
1. NASA, Ames Research Center, Moffett Field, CA
2. Informatics, Inc., Palo Alto, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1056
Reference24 articles.
1. 'Henees, G. P. "Thermal Protection Requirements for Near-Earth Aeroassisted Orbital Transfer Vehicle Missions," AIAA Paper 83-1513,1983.
2. 'Leiser, D. 8.Goldstien, H. E., and Smith, M. "Fibrous Refractory Composite Insulation,"U.S. Patent No. 4,148,962, 1978.
3. 5Leiser, D. B., Stewart, D. A, and Smith,M. "Advances in TPS and Structures for Space Transportation Systems,''NASA CP-2315, 1983.
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