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Conic solutions to the interplanetary transfer problem with constant or minimum injection energyMinimum and constant energy values for injection into launch window to achieve interplanetary spacecraft trajectory
Document ID
19650026376
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Bullock, L. E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
August 16, 1965
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-53319
Report Number: NASA-TM-X-53319
Accession Number
65N35977
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPACECRAFT TRAJECTORY
INJECTION
INTERPLANETARY TRAJECTORY
LAUNCH WINDOW

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