Gaseous propellants exhibit large variations in pressure and temperature and hence in fuel delivery. All-mechanical, mass flow controller which compensates for these variations has been developed to maintain constant fuel rate of gas. Further work is necessary to ease inlet pressure limitation.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Mass flow controller for gaseous propellants


    Publication date :

    1973-06-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Ignition System for Gaseous Propellants

    Pieron, R. A. | NTRS | 1986


    Breakdown Voltage Determination for Gaseous and Cryogenic Propellants

    Nugent, Nicholas / Helderman, David / Boopalan, Avanthi et al. | AIAA | 2007


    Breakdown Voltage Determination for Gaseous and Cryogenic Propellants AIAA Paper

    Nugent, N. / Helderman, D. / Boopalan, A. et al. | British Library Conference Proceedings | 2007


    Isolated Ground Return Electrode for Use in Gaseous and Cryogenic Propellants

    Nugent, Nicholas / Helderman, David / Anderson, William | AIAA | 2008


    Capacitance mass sensing of boiling propellants

    Perkins, C. K. / Wilburn, R. D. | NTRS | 1964