Effects of environmental and ablator performance uncertainties on heat-shielding requirements for hyperbolic entry vehicles.
- 1 November 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (11) , 1260-1270
- https://doi.org/10.2514/3.29467
Abstract
No abstract availableKeywords
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