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- W2318676414 abstract "The atmospheric flight environment of manned return from Mars is evaluated by analyzing the earth-return entry corridor. To identify and quantify the effects of various atmospheric exit conditions on the mission, the differences beween the capture to a specific orbit and the direct entry to a target splashdown site are investigated. The differences are quantified in terms of the airbrake lift-drag ratio requirements, the stagnation-point heating, and the significance of off-nominal atmospheric conditions. Results are presented on three different earth-return aerobraking scenarios: (1) the capture into a phasing orbit with a 24-hr period, (2) the capture into a 500-km circular orbit, and (3) the direct entry to splashdown." @default.
- W2318676414 created "2016-06-24" @default.
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- W2318676414 date "1991-08-12" @default.
- W2318676414 modified "2023-09-23" @default.
- W2318676414 title "Earth aerobraking strategies for manned return from Mars" @default.
- W2318676414 doi "https://doi.org/10.2514/6.1991-2873" @default.
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