A method for the conceptual design of a capsule type re-entry vehicle was investigated aerodynamically and aerothermodynamically. The purpose of this investigation was to find a method for determining the optimum thermal protection thickness under arbitrary constraints such as decelaration rate, down range, and so forth.
Method for Aerodynamic and Aerothermodynamic Conceptual Design of Capsule Type Re-entry Vehicle
1983
80 pages
Report
Keine Angabe
Englisch
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