Heat-transfer distributions on biconics at incidence in hypersonic-hypervelocity He, N2, air, and CO2 flows
Author:
Affiliation:
1. NASA, LangelyResearch Center, Space Systems Div., Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1983-1508
Reference41 articles.
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3. 3Florence, D. E. "Aerothermodynamic Design Feasibility of a Generic Planetary Aerocapture/ Aeromaneuver Vehicle," AIAA Paper 81-1127, June 11181.
4. 'Austin, R. E., Cruz, M. I., and French, J. R. "System Design Concepts and Requirements for Aeroassisted Orbital Transfer Vehicles,'I AlAA Paper 82-1379, August 1982.
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4. A survey of aeroassisted orbit transfer;Journal of Spacecraft and Rockets;1985-01
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