Optimum configuration of high-lift aeromaneuvering orbital transfer vehicles in viscous flow
Author:
Affiliation:
1. Informatics General Corp., Palo Alto, CA
2. NASA, Ames Research Center, Moffett Field, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1059
Reference17 articles.
1. Aerodynamic characteristics of generalized bent biconic bodies for aero-assisted, orbital-transfer vehicles
2. A review of aeroassisted orbit transfer
3. 3Menees, G. P. "Thermal-protectionRequirements for Near-Earth Aeroassisted Orbital Transfer Vehicle Missions," AIAA Paper 83-1573,Jan. 1983 (also to be published in the 1984 Thermophysics Volume of the AIAA Progress Series).
4. 'Menees, G. P. and Park, C. "Design and Performance Analysis of a Conical Aerobrake Orbital Transfer Vehicle Concept," AIAA Paper 84-0410,Jan. 1984 (also to be published in the 1984 Thermophysics Volume of the AIAA Progress Series).
5. 5Menees,G. P., Davies,C. B., and Wilson, J. F. "AerothermodynamicHeating Analysis of Aerobraking and Aeromaneuvering Orbit-Transfer Vehicles," AIAA Paper 84-1711,June 1984 (also to be published in the 1984 Thermophysics Volume of the AIAA Progress Series).
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1. Atmospheric environment during maneuvering descent from Martian orbit;Journal of Spacecraft and Rockets;1989-09
2. Optimum configuration of high-lift aeromaneuvering orbital transfer vehicles in viscous flow;Journal of Spacecraft and Rockets;1988-05
3. Aerothermodynamic heating and performance analysis of a high-lift aeromaneuvering AOTV concept;Journal of Spacecraft and Rockets;1987-05
4. Chemical and Thermal Nonequilibrium Heat-Transfer Analysis for Hypervelocity, Low Reynolds Number Flow;Thermophysical Aspects of Re-Entry Flows;1986-01-01
5. Chemical and thermal nonequilibrium heat transfer analysis for hypervelocity, low Reynolds number flow;20th Thermophysics Conference;1985-06-19
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