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TRAJECTORIES LAUNCHED NORMAL TO THE ECLIPTICOne-dimensional approximate analysis of the motion of a vehicle launched normal to the ecliptic at relatively low escape speed
Document ID
19630029612
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Breakwell, J. V.
Date Acquired
August 1, 2013
Publication Date
October 1, 1963
Subject Category
Space Radiation
Report/Patent Number
IAF PAPER 67
Report Number: IAF PAPER 67
Accession Number
63A25671
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY
SPACECRAFT TRAJECTORY

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