Pressure fed fluorine-oxidized rocket propulsion systems offer payload increases of 25 to 110% over payload of equivalent oxygen oxidized systems, depending on, and increasing with upper stage velocity requirement, such that payload increase of 100% can be estimated for lunar or planetary missions; phased tripropellant fluorine-propulsion system concept is introduced; measure of current state of art of these systems is presented relating to development and operational experience gained in 800 fluorine propulsion subsystems tests conducted during past 6 yr.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Fluorine-oxidized rocket systems for space propulsion


    Weitere Titelangaben:

    ASME -- Paper


    Beteiligte:
    Carey, L. (Autor:in)

    Kongress:

    ASME Meeting AHGT-96 ; 1963 Propellants



    Erscheinungsdatum :

    1963


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Non-Rocket In-Space Propulsion

    Vulpetti, Giovanni / Johnson, Les / Matloff, Gregory L. | Springer Verlag | 2008


    Propulsion for space - The nuclear rocket.

    Johnson, P. G. / Schwenk, F. C. | NTRS | 1967


    Solid Rocket and Space Propulsion Studies

    R. L. Glick / J. R. Osborn | NTIS | 1984


    Rocket space propulsion in 1970's

    Cumming, J.M. | Engineering Index Backfile | 1968


    Rocket propulsion

    Dunn, L.G. | Engineering Index Backfile | 1947