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Mars trajectory options for the Space Exploration InitiativeThe 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.
Document ID
19920060739
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Soldner, John K.
(Science Applications International Corp. Human Spaceflight and Exploration Div., Houston, TX, United States)
Joosten, B. K.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 91-438
Meeting Information
Meeting: AAS/AIAA Astrodynamics Conference
Location: Durango, CO
Country: United States
Start Date: August 19, 1991
End Date: August 22, 1991
Accession Number
92A43363
Distribution Limits
Public
Copyright
Other

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