THERMAL PROTECTION SYSTEM PERFORMANCE OF THE APOLLO COMMAND MODULE
- 18 April 1966
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Design of ablative thrust chambers and their materialsJournal of Spacecraft and Rockets, 1965
- EXPERIMENTAL INVESTIGATION OF A CHARRING ABLATIVE MATERIAL EXPOSED TO COMBINED CONVECTIVE AND RADIATIVE HEATING IN OXIDIZING AND NONOXIDIZING ENVIRONMENTSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1964
- CONSTANT CONVECTIVE HEATING RATE SURFACES FOR LIFTING RE-ENTRY VEHICLESAIAA Journal, 1963