This paper describes an advanced development program for the demonstration of the aerospike rocket engine system. This three-task, 31-month program consists of the analytical and design studies to be accomplished under Task I; aerospike thrust chamber experimental segment testing to be accomplished under Task II; and demonstration of the full aerospike thrust chamber to be accomplished under Task III. The program is being conducted at Rocketdyne, a division of North American Rockwell Corporation, under the sponsorship of the Air Force Rocket Propulsion Laboratory under Contract F04611-67-C-0116. This paper summarizes the accomplishments of the program to date, and describes the engine system and its possible application to the orbit-to-orbit shuttle (OOS).


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A Propulsion System for Orbit-to-Orbit Shuttle


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Lamont, E. A. (Autor:in) / Wells, W. W. (Autor:in)

    Kongress:

    National Aeronautical and Space Engineering and Manufacturing Meeting ; 1971



    Erscheinungsdatum :

    01.02.1971




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :