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FREE RETURN CIRCUMLUNAR TRAJECTORIES FROM LAUNCH WINDOWS WITH FIXED LAUNCH AZIMUTHSFactors affecting free return circumlunar trajectories from launch windows with fixed launch azimuths, emphasizing effects of parking orbit launch time
Document ID
19630028267
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Johnson, F., Jr.
Date Acquired
August 1, 2013
Publication Date
August 21, 1963
Subject Category
Space Radiation
Report/Patent Number
AIAA PAPER 63-406
Report Number: AIAA PAPER 63-406
Accession Number
63A24326
Distribution Limits
Public
Copyright
Other
Keywords
TRAJECTORY
CIRCUMLUNAR TRAJECTORY
ORBITAL MECHANICS

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