Chemical nonequilibrium effects on flowfields for aeroassisted orbital transfer vehicles
- 1 January 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 22 (1) , 54-59
- https://doi.org/10.2514/3.25709
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- System design concepts and requirements for aeroassisted orbital transfer vehiclesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Viscous-shock-layer heating analysis for the shuttle windward-symmetry plane with surface finite catalytic recombination ratesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Aerobraked orbital transfer vehicle definitionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Flow field investigation of atmospheric braking for high drag vehicles with forward facing jetsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- Is a versatile orbit transfer stage feasibleOrbit Transfer Vehicle concepts, potential missions and evolutionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Numerical solution of the hypersonic viscous shock-layer equationsAIAA Journal, 1970