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Selection process for trade study: Reusable Hydrogen Composite Tank System (RHCTS)This document describes the selection process that will be used to identify the most suitable structural configuration option for an SSTO winged vehicle capable of delivering 25,000 lbs to a 220 nm circular orbit at 51.6 degree inclination. The most suitable RHCTS is within this configuration and will be the prototype design for subsequent design and analysis and the basis for the design and fabrication of a scale test article to be subjected to life cycle testing. The selection process for this TA 1 trade study is the same as that for the TA 2 trade study. As the trade study progresses additional insight may result in modifications to the selection criteria within in this process. Such modifications will result in an update of this document as appropriate.
Document ID
19950005396
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Greenberg, H. S.
(Rockwell International Corp. Downey, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 2, 1994
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
NASA-CR-196874
NAS 1.26:196874
SSD94D0209
Report Number: NASA-CR-196874
Report Number: NAS 1.26:196874
Report Number: SSD94D0209
Accession Number
95N11809
Funding Number(s)
CONTRACT_GRANT: NCC8-39
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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