The results of a study to the validate the applicability of the aerobraking concept to the SOCCER (sample of comet coma earth return) mission using a six-DOF computer simulation of the aerobraking process are presented. The SOCCER spacecraft and the aerobraking scenario and power supply problem are briefly described. Results are presented for the spin effect, payload exposure problem, and sun angle effect.
Aerobraking strategies for the sample of comet coma earth return mission
International Symposium on Space Technology and Science ; 1990 ; Tokyo, Japan
01.01.1990
Aufsatz (Konferenz)
Keine Angabe
Englisch
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