With reusability accepted as a means of reducing operating costs, the size of the initial investment (research and development) is likely to determine the choice for the next generation boosters. High volume utilisation lifting bodies propelled by LH/LOX rockets in a vertical take-off mode are shown to be superior to several other concepts. This is largely due to the low manufactured weight without undue complexity or use of exotic materials, leading to low R&D and low unit cost.Even lower costs can be shown for a modular concept (MUSTARD) in which basically identical lifting bodies units are utilised as both boosters and spacecraft. The concept is shown to be feasible, and progress on some aspects of the associated structural analysis is described.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    A British Reusable Booster Concept


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Smith, T. W. (Autor:in)

    Kongress:

    Space Technology Conference ; 1967



    Erscheinungsdatum :

    01.02.1967




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    British reusable booster concept

    Smith, T.W. | Engineering Index Backfile | 1967


    REUSABLE BOOSTER ROCKET

    SUSHENTSEV BORIS NIKIFOROVICH | Europäisches Patentamt | 2020

    Freier Zugriff

    EELV Partially Reusable Booster

    Gravlee, M. / Zegler, F. / Bulk, T. et al. | British Library Conference Proceedings | 2010


    Experimental Investigation of a Suborbital Reusable Booster Concept with Canards

    Post, Martiqua / Dobransky, Michael / Shackelford, William et al. | AIAA | 2011


    EXPERIMENTAL INVESTIGATION OF A SUBORBITAL REUSABLE BOOSTER CONCEPT WITH CANARDS

    Post, M. / Dobransky, M. / Shackelford, W. et al. | British Library Conference Proceedings | 2011