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Preliminary analysis of STS-3 entry flight dataThe primary test objectives of STS 3 entry were to gather additional stability and control data at the higher Mach numbers and to expand the autoland operational envelope down to 200 feet. A time history of the entire entry and a list of the significant test conditions are shown. The weight, cg, and inertia characteristics used in the analyses are also shown.
Document ID
19820023528
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Date Acquired
September 4, 2013
Publication Date
August 1, 1982
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-TM-81373
NAS 1.15:81373
Report Number: NASA-TM-81373
Report Number: NAS 1.15:81373
Accession Number
82N31404
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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