A configuration for re-entry from mars missions using aerobraking
- 1 July 1965
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 2 (4) , 501-507
- https://doi.org/10.2514/3.28219
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Velocity requirements and re-entry flight mechanics for manned mars missionsJournal of Spacecraft and Rockets, 1964
- Factors influencing configuration and performance of multipurpose manned entry vehiclesJournal of Spacecraft and Rockets, 1964
- RADIANCE OF SPECIES IN HIGH TEMPERATURE AIRPublished by Defense Technical Information Center (DTIC) ,1963
- Heat Transfer in Planetary Atmospheres at Super-Satellite SpeedsARS Journal, 1962
- Thermal Degradation of a Char-Forming Plastic During Hypsersonic FlightARS Journal, 1962
- Laminar Heat Transfer Over Blunt-Nosed Bodies at Hypersonic Flight SpeedsJournal of Jet Propulsion, 1956