Applications comprise auxiliary power units in missiles, aircraft and space vehicles; factors to consider; propellant properties; process flow outline for production, process and quality control techniques applied at North American Aviation; purpose and design of Tartar and Terrier gas generator, liquid engine turbine starter and jet engine starter cartridge, pointing out problem areas; future developments.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Development and tests for achieving reliability and reproducibility of solid propellant gas generators


    Additional title:

    SAE -- Paper


    Contributors:

    Conference:

    SAE Meeting ; 1960 Auxiliary power systems



    Publication date :

    1960


    Size :

    12 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English





    Minimum-Response-Delay Controllable Solid-Propellant Gas Generators

    J. Cohen / L. C. Landers / R. L. Lou | AIAA | 1977


    Zero time delay controllable solid propellant gas generators

    COHEN, J. / LANDERS, L. / LOU, R. | AIAA | 1976


    P4S-1 Solid Propellant Pulsed Plasma Thruster - Development Tests

    Brito, Hector H. / De Alessandro, Roque / Dominguez, Carlos et al. | AIAA | 2006


    Fire suppression in aircraft by solid propellant gas generators

    Lemke, Jens / Beuermann, Rainer / Meyer, Michael | Tema Archive | 2013