Effects of environmental and ablator performance uncertainties on heat-shielding requirements for hyperbolic entry vehicles.
Author:
Affiliation:
1. Lockheed Missiles & Space Company, Sunnyvale, Calif.
2. NASA Ames Research Center, Moffett Field, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.29467
Reference25 articles.
1. Hearne, L. F. etal. "A Study of the Effects of Environmental and Ablator Performance Uncertainties on Heat Shielding Requirements for Hyperbolic Entry Vehicles," CR-73224 1968 NASA.
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