ENTRY AND LANDING REQUIREMENTS FOR MANNED PLANETARY MISSIONS
- 4 March 1968
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
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- Laminar convective heating and ablation in the Mars atmosphere.AIAA Journal, 1967
- Convective and radiative heat transfer during superorbital entry.AIAA Journal, 1967
- Boundary-layer transition on ablating cones at speeds up to 7 km/sec.AIAA Journal, 1966
- THERMAL PROTECTION SYSTEM PERFORMANCE OF THE APOLLO COMMAND MODULEPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1966
- Experimental investigation of a charring ablative material exposed to combined convective and radiative heating.AIAA Journal, 1965
- Studies of shock-layer radiation of bodies entering planetary atmospheres.AIAA Journal, 1965
- Venus swingby mode for manned mars missionsJournal of Spacecraft and Rockets, 1964
- Experimental study of radiative transport from hot gases simulating in composition the atmospheres of mars and venusAIAA Journal, 1964
- ATMOSPHERE ENTRY PROBLEMS OF MANNED INTERPLANETARY FLIGHTPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1963