Heating analysis for a Lunar Transfer Vehicle at near-equilibrium flow conditions
- 11 January 1993
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 6 references indexed in Scilit:
- A parametric analysis of radiative structure in aerobrake shock layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Coupled radiation effects in thermochemical nonequilibrium shock-capturing flowfield calculationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1992
- Computation of near-wake, aerobrake flowfieldsJournal of Spacecraft and Rockets, 1992
- Navier-Stokes and viscous shock-layer solutions for radiating hypersonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- Thermal response of integral multicomponent composite thermal protection systemsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Fully coupled nongray radiating gas flows with ablation product effects about planetary entry bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973