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A preliminary analysis of a three impulse technique for transearth injection from highly inclined orbitsPreliminary analysis of three impulse technique for transearth injection from highly inclined orbits
Document ID
19680020034
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Webb, E. D. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 4, 2013
Publication Date
May 24, 1966
Subject Category
Space Sciences
Report/Patent Number
LMSC-A822605
NASA-CR-92164
Report Number: LMSC-A822605
Report Number: NASA-CR-92164
Accession Number
68N29506
Funding Number(s)
CONTRACT_GRANT: NAS9-5288
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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