Aerothermodynamic characteristics of slender ablating re-entry vehicles
- 1 April 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 8 (4) , 373-380
- https://doi.org/10.2514/3.30281
Abstract
No abstract availableKeywords
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