The Mission Definition Office within the Lunar and Mars Exploration Program Office at the NASA/Johnson Space Center has the responsibility for leading the Space Exploration Initiative mission design activities across the Agency. In support of the Synthesis Group architecture analyses, a mission concept that includes fast one-way transits to and from Mars, a powered flyby abort, and an early return option has been developed. This paper will describe this integrated approach to Mars mission planning.
Mars trajectory options for the Space Exploration Initiative
AAS/AIAA Astrodynamics Conference ; 1991 ; Durango, CO, United States
1992-01-01
Conference paper
No indication
English
Single-Cycler Trajectory Options for Mars Exploration
AIAA | 2017
|Single-Cycler Trajectory Options for Mars Exploration (AIAA 2017-5282)
British Library Conference Proceedings | 2017
|NTRS | 1974
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