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Mission Design for Mars Missions Using the Ariane ASAP Launch CapabilityThese missions are made possible with the use of the MEGA process, which will be discussed here in some detail.
Document ID
20210002755
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/16879
Authors
Penzo, P.
Date Acquired
February 7, 1999
Publication Date
February 7, 1999
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Mars
Mission
Ariane
launch
window
secondary
payloads

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