Technological requirements and forecasts of rocket engine parameters and launch vehicles for future Earth to geosynchronous orbit transportation systems are presented. The parametric performance, weight, and envelope data for the LOX/CH4, fuel cooled, staged combustion cycle and the hydrogen cooled, expander bleed cycle engine concepts are discussed. The costing methodology and ground rules used to develop the engine study are summarized. The weight estimating methodology for winged launched vehicles is described and summary data, used to evaluate and compare weight data for dedicated and integrated O2/H2 subsystems for the SSTO, HLLV and POTV are presented. Detail weights, comparisons, and weight scaling equations are provided.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Technology Requirements for Future Earth-to-Geosynchronous Orbit Transportation Systems. Volume 3: Appendices


    Beteiligte:
    V. A. Caluori (Autor:in) / R. T. Conrad (Autor:in) / J. C. Jenkins (Autor:in)

    Erscheinungsdatum :

    1980


    Format / Umfang :

    146 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch