Publication Date:
2019-07-13
Description:
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.
Keywords:
ASTRODYNAMICS
Type:
International Symposium on Space Technology and Science; May 20, 1990 - May 25, 1990; Tokyo; Japan
Format:
text
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