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EGO orbital parameters and heat inputsComputation methods and results for orbital data, spacecraft angle, and heat input for OGO AND specifically for EGO
Document ID
19660011717
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Montgomery, H. E. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Paddack, S. J. (NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1963
Subject Category
Space Sciences
Report/Patent Number
NASA-TM-X-55428
X-643-63-61
NSSDC-ID-64-054A-00-PM
Report Number: NASA-TM-X-55428
Report Number: X-643-63-61
Report Number: NSSDC-ID-64-054A-00-PM
Accession Number
66N21006
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SPACECRAFT
HEAT GAIN
ORBITAL CALCULATION
OGO

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