Application of PLCs to the rocket engine component testing at a new Stennis Space Center Component Test Facility is suggested as an alternative to dedicated specialized computers. The PLC systems are characterized by rugged design, intuitive software, fault tolerance, flexibility, multiple end device options, networking capability, and built-in diagnostics. A distributed PLC-based system is projected to be used for testing LH2/LOx turbopumps required for the ALS/NLS rocket engines.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    The use of programmable logic controllers (PLC) for rocket engine component testing


    Beteiligte:
    Nail, William (Autor:in) / Scheuermann, Patrick (Autor:in) / Witcher, Kern (Autor:in)

    Erscheinungsdatum :

    01.06.1991


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    The use of programmable logic controllers (PLC) for rocket engine component testing

    NAIL, WILLIAM / SCHEUERMANN, PATRICK / WITCHER, KERN | AIAA | 1991



    Testing embedded engine controllers using programmable test techniques

    DeKoeklkock,R.J. / DePaula,R.I. / Richardson,D.J. et al. | Kraftfahrwesen | 2005


    Testing Embedded Engine Controllers Using Programmable Test Techniques

    Richardson, Daniel J. / DePaula, Roberto I. / DeKoekkoek, Ronald J. | SAE Technical Papers | 2005


    Modeling Programmable Logic Controllers for Logic Verification

    Moon, I. | British Library Online Contents | 1994