This paper describes the analysis and results of an investigation of the Mars Rover/Sample Return mission's landing strategy, together with the trade-offs of different landing strategies. The percentile points and the descriptive statistics of the probability distribution of traverse distances are calculated using a simple model formulated on the basis of landing error characteristics. The results show that variations in the landing stratgegy can significantly affect the traverse distance requirements, which range from 20 to 200 km.
Mars Rover/Sample Return landing strategy
AAS/AIAA Astrodynamics Conference ; 1987 ; Kalispell, MT, United States
1988-01-01
Conference paper
No indication
English
Mars Rover Sample Return - Rover challenges
AIAA | 1988
|Mars Rover Sample Return - Rover challenges
NTRS | 1988
|Mars rover sample return missions
NTRS | 1988
|Mars Rover Sample Return Mission
NTRS | 1988