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Sa-8 operational trajectoryTrajectory optimization for Saturn I /SA-8/ LAUNCH vehicle to place S- IV stage and payload in elliptical orbit
Document ID
19650014195
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Pack, P. B. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Solmon, G. W. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
May 17, 1965
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-53262
Accession Number
65N23796
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SATURN I /SA-8/ LAUNCH VEHICLE
SATURN S-IV STAGE
ELLIPTICAL ORBIT
TRAJECTORY OPTIMIZATION

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