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    Cycle O (CY 1991) NLS trade studies and analyses, book 2. Part 1: Avionics and systems (1992)
    In:  CASI
    Details
    Publication Date: 2019-07-13
    Description: An assessment was conducted to determine the maximum LH2 tank stretch capability based on the constraints of the manufacturing, tooling and facilities at the Michoud Assembly Facility in New Orleans, Louisiana. The maximum tank stretch was determined to be 5 ft. with minor or no modifications, a stretch of 11 ft. with some possible facility modifications and beyond 11 ft. significant new facilities are required. A cost analysis was performed to evaluate the impacts for various stretch lengths. Tasks that were defined to perform trades and studies regarding the best approach to meet requirements for the National Launch System Avionics are also discussed.
    Keywords: ENGINEERING (GENERAL)
    Type: NASA-CR-184472-BK-2-PT-1 , NAS 1.26:184472-BK-2-PT-1 , MMC-NLS-SR.001-BK-2-PT-1
    Format: application/pdf
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