A concept for a lightweight space-based orbital transfer vehicle (OTV) featuring thin, spherical, pressure-designed aluminum liquid-oxygen and liquid-hydrogen tanks and a truss structure of composite materials is used as a baseline design for a large-cargo OTV. Vehicle sizing, fleet analysis, and parametric cost analysis are used to evaluate the effects of engine technology, vehicle staging, and high-thrust versus low-thrust transfer. Results indicate that Earth-to-orbit launch costs and OTV engine performance are strong drivers in orbital transportation cost and that there is no significant benefit in staging vehicles. At the low values of Earth-to-orbit cost representative of advanced launch vehicles, low-thrust and high-thrust OTV's are competitive.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Propulsion options for space-based orbital transfer vehicles


    Beteiligte:
    Rehder, J. J. (Autor:in) / Wurster, K. E. (Autor:in) / Macconochie, I. O. (Autor:in) / Klich, P. J. (Autor:in)

    Kongress:

    Joint Propulsion Conference ; 1978 ; Las Vegas, NV, US


    Erscheinungsdatum :

    1978-07-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Propulsion Options for Space-Based Orbital Transfer Vehicles

    John J. Rehder / Kathryn E. Wurster / lan O. MacConochie et al. | AIAA | 1979


    Propulsion options for space-based orbital transfer vehicles

    REHDER, J. / WURSTER, K. / MACCONOCHIE, I. et al. | AIAA | 1978


    Paste Propulsion of Space Transportation Vehicles for Orbital Transfer Applications

    Babuk, V. A. / Budnyi, N. L. / Naryzhnyi, S. Yu. | Springer Verlag | 2023