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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    High frequency data acquisition system for space shuttle main engine testing


    Contributors:


    Publication date :

    1987-10-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English





    Space Shuttle Main Engine

    Thompson, J. R., Jr. | NTRS | 1977


    Space Shuttle Main Engine control system

    Seitz, P. F. / Searle, R. F. | NTRS | 1973


    Space Shuttle Main Engine Control System

    Seitz, P. F. / Searle, R. F. | SAE Technical Papers | 1973