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Trajectory design for impulsive Earth-Mars- Earth trajectories launched in 1969 and 1971.Trajectory design for spacecraft which returns in vicinity of earth after Mars encounter analyzed by patched conic model
Document ID
19670041256
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Feitis, P. H.
Date Acquired
August 3, 2013
Publication Date
July 1, 1966
Subject Category
Space Sciences
Report/Patent Number
AAS PAPER 66-126
Report Number: AAS PAPER 66-126
Accession Number
67A19985
Distribution Limits
Public
Copyright
Other
Keywords
PLANETARY SPACECRAFT
SPACECRAFT TRAJECTORY
EARTH-MARS RENDEZVOUS TRAJECTORY

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