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Optimal finite-thrust transfer between planet approach and departure asymptotes with specified intermediate orbitOptimal finite-thrust transfer between planet approach and departure asymptotes with specified intermediate orbit
Document ID
19680012627
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Willis, E. A., Jr. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TN-D-4534
Accession Number
68N22096
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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