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OFT-1 reference flight profile. Deorbit through landingChanges made in the de-orbiting through landing reference flight profile because of increases in Orbiter weight during entry and in the circular orbital attitude prior to deorbit are discussed. The rationale for the shaping of each phase is also presented.
Document ID
19770024271
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Heath, D. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Gonzales, L. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Montez, M. (NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Hiott, J. M. (McDonnell Douglas Tech. Service Co., Inc.)
Ruda, R. (McDonnell Douglas Tech. Service Co., Inc.)
Kyle, H. (McDonnell Douglas Tech. Service Co., Inc.)
Date Acquired
September 3, 2013
Publication Date
August 1, 1977
Subject Category
Astronautics (General)
Report/Patent Number
REPT-77-FM-36
JSC-12957
NASA-TM-74939
Report Number: REPT-77-FM-36
Report Number: JSC-12957
Report Number: NASA-TM-74939
Accession Number
77N31215
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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