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.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    High frequency data acquisition system for space shuttle main engine testing


    Beteiligte:
    Lewallen, Pat (Autor:in)


    Erscheinungsdatum :

    1987-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    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