The search for optimum configurations for re-entry vehicles
Author:
Affiliation:
1. TRW Electronics and Defense Sector, San Bernardino, California
2. Ballistic Missile Office, Norton AFB, San Bernardino, California
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.8625
Reference27 articles.
1. Optimum body geometries of minimum heat transfer at hypersonic speeds.
2. Baker, R. L. and Kramer, R. F. "Reentry Vehicle Nosetip Design for Minimum Total Heat Transfer," AIAA Paper 79-201, New Orleans, La., Jan.1979.
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