A preliminary TPS design for MRSR - Aerobraking at Mars and at earth
- 8 January 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Comparison of viscous shock layer and boundary layer reentry heatingtechniques for Orbiter nose capPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986