Optimization of aerobraked orbital transfer vehicles
Author:
Affiliation:
1. Boeing Aerospace Co., Seattle, WA
2. Goodyear Aerospace Corp., Akron, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1981-1126
Reference4 articles.
1. Aerobraked orbital transfer vehicle definition
2. Bartle. E.R., and Leadon,B.M."The Effectiveness the 1962 Heat Transfer and Fluid Mechanics-Institute, June 13-15, 1962.
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1. Theory of idealized two-dimensional ballute in Newtonian hypersonic flow;Journal of Spacecraft and Rockets;1988-05
2. A survey of aerobraking orbital transfer vehicle design concepts;25th AIAA Aerospace Sciences Meeting;1987-03-24
3. Heating distribution comparison between asymmetric and symmetric blunt cones;4th Thermophysics and Heat Transfer Conference;1986-06-02
4. Theory of idealized two-dimensional ballute in Newtonian hypersonic flow;24th Aerospace Sciences Meeting;1986-01-06
5. Aerodynamics of generalized bent biconics for aero-assisted, orbital-transfer vehicles;Journal of Spacecraft and Rockets;1985-03
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