Propellants having the combustion efficiency and high burning rates normally only achieved with perchlorates, have now been formulated with ammonium nitrate as the primary oxidizer, and with powdered metal fuel, all of which permits the use of lesser amounts of perchlorate oxidizer. These novel formulations greatly reduce the total hydrogen chloride emissions to the atmosphere, and hence are particularly desirable for the Space Shuttle propulsion systems.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    High Performance Ammonium Nitrate Propellant


    Beteiligte:
    F. A. Anderson (Autor:in)

    Erscheinungsdatum :

    1977


    Format / Umfang :

    26 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Evaluation of Ammonium Nitrate Propellant Emissions

    Stowe, R. A. / Lessard, P. / Roy, G. et al. | British Library Conference Proceedings | 1995


    Ballistic range performance of ammonium nitrate-alcohol (ANA) propellant

    Sasoh, A. / Ogawa, T. / Takayama, K. et al. | AIAA | 1999


    Ammonium nitrate-magnesium propellant combustion and heat transfer mechanisms

    BREWSTER, M. Q. / SHERIDAN, TODD A. / ISHIHARA, ATSUSHI | AIAA | 1992


    Ammonium nitrate-magnesium propellant combustion and heat transfer mechanisms

    BREWSTER, M. / SHERIDAN, TODD / ISHIHARA, ATSUSHI | AIAA | 1991


    Electrolytic Combustion in the Polyvinyl Alcohol + Hydroxyl Ammonium Nitrate Solid Propellant

    Baird, James / Lang, Joshua / Hiatt, Andrew et al. | AIAA | 2016