Aerothermodynamic design feasibility of a Mars aerocapture/aeromaneuver vehicle
- 12 January 1981
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Selection, development, characterization and flight test of a thermal protection system for an earth entry satellite vehiclePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978