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Launch vehicle error sensitivity studyBooster trajectory optimization for launch vehicle range sensitivity analysis
Document ID
19700009457
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rosenbaum, R. C. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Willwerth, R. E. (Lockheed Missiles and Space Co. Sunnyvale, CA, United States)
Date Acquired
August 6, 2013
Publication Date
February 1, 1970
Publication Information
Publisher: NASA
Subject Category
Navigation
Report/Patent Number
NASA-CR-1512
Report Number: NASA-CR-1512
Accession Number
70N18762
Funding Number(s)
CONTRACT_GRANT: NAS1-8920
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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