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LAUNCH WINDOW STUDIES EMPLOYING VARIATIONAL CALCULUS TO DETERMINE OPTIMUM THREE DIMENSIONAL TRAJECTORIES LEADING TO INJECTION INTO A SPACE-FIXED CIRCULAR ORBITDetermination of optimum 3-dimensional trajectories to inject a saturn c-5 rocket into a space-fixed circular orbit
Document ID
19630016000
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Miner, W. E.
Silber, R.
Date Acquired
August 1, 2013
Publication Date
November 18, 1962
Subject Category
Space Radiation
Report/Patent Number
ARS PAPER 62-2626
Report Number: ARS PAPER 62-2626
Accession Number
63A12059
Distribution Limits
Public
Copyright
Other
Keywords
SPACECRAFT TRAJECTORY
SATURN V LAUNCH VEHICLE
SATELLITE ORBIT

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