Selection of a heat protection system for Venusian entry
Author:
Affiliation:
1. General Electric Co., Re-Entry and Environmental Systems Div., Philadelphia, Pa.
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1975-731
Reference12 articles.
1. Laminar Heat Transfer on Three-Dimensional Blunt Nosed Bodies in Hypersonic Flow
2. An approximate inviscid radiating flow-field analysis for sphere-cone Venusian entry vehicles
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2. Aerothermodynamic Design Feasibility of a Generic Planetary Aerocapture/Aeromaneuver Vehicle;Thermophysics of Atmospheric Entry;1982-01-01
3. Aerothermodynamic design feasibility of a generic planetary aerocapture/aeromaneuver vehicle;16th Thermophysics Conference;1981-06-23
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