Aerothermodynamic environments for Mars entry, Mars return, and lunar return aerobraking missions
- 18 June 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 13 references indexed in Scilit:
- A preliminary TPS design for MRSR - Aerobraking at Mars and at earthPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- The use of atmospheric braking during Mars missionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Development of AFE aerobrake aerothermodynamic data bookPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- Aerobrake heating rate sensitivity study for the Aeroassist Flight Experiment (AFE)Published by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- The effect of electron temperature and impact ionization on Martian return AOTV flowfieldsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1989
- The computation of radiation from nonequilibrium hypersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Nitrogen recombination on high-temperature reusable surface insulation and the analysis of its effect on surface catalysisPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Fully coupled nongray radiating gas flows with ablation product effects about planetary entry bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Radiative and convective heating during Venus entry.AIAA Journal, 1972
- Effects of non-grey self-absorption and energy loss for blunt body flowsJournal of Quantitative Spectroscopy and Radiative Transfer, 1968