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Nozomi CIS-Lunar Phase Orbit DeterminationThe Nozomi spacecraft is the first to achieve an Earth-Mars transfer orbit without a direct hyperbolic insertion maneuver.
Document ID
20210003007
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/17971
Authors
Criddle, K.
Ryne, M.
Date Acquired
August 16, 1999
Publication Date
August 16, 1999
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Nozomi
Planet-B
Orbit
Determination

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