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    High frequency data acquisition system for space shuttle main engine testing (1987)
    In:  CASI
    Details
    Publication Date: 2013-08-31
    Description: The high frequency data acquisition system developed for the Space Shuttle Main Engine (SSME) single engine test facility at the National Space Technology Laboratories is discussed. The real time system will provide engineering data for a complete set of SSME instrumentation (approx. 100 measurements) within 4 hours following engine cutoff, a decrease of over 48 hours from the previous analog tape based system.
    Keywords: SPACECRAFT PROPULSION AND POWER
    Type: The 58th Shock and Vibration Symposium, Volume 1; p 349-352
    Format: application/pdf
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