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Venus and Beyond Using the Ariane ASAP Launch CapabilityA general trajectory scenario has been designed which can transfer a spacecraft from a pre-specified, highly eccentric, near equatorial orbit to a desired escape direction.
Document ID
20210003005
Acquisition Source
Jet Propulsion Laboratory
Document Type
Other
External Source(s)
hdl:2014/17941
Authors
Penzo, P.
Date Acquired
August 16, 1999
Publication Date
August 16, 1999
Publication Information
Publisher: UNKNOWN
Distribution Limits
Public
Copyright
Other
Technical Review
Keywords
Venus
Ariane
Secondary
Payloads
Launch
Trajectories

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