The use of hydrogen RP-1, propane, and methane as fuels for booster engines of launch vehicles is discussed. An automated procedure for integrated launch vehicle, engine sizing, and design optimization was used to define two stage and single stage concepts for minimum dry weight. The two stage vehicles were unmanned and used a flyback booster and partially reusable orbiter. The single stage designs were fully reusable, manned flyback vehicles. Comparisons of these vehicle designs, showing the effects of using different fuels, as well as sensitivity and trending data, are presented. In addition, the automated design technique utilized for the study is described.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Booster Propulsion/Vehicle Impact Study


    Beteiligte:
    V. Weldon (Autor:in) / M. Dunn (Autor:in) / L. Fink (Autor:in) / D. Phillips (Autor:in) / E. Wetzel (Autor:in)

    Erscheinungsdatum :

    1988


    Format / Umfang :

    574 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Booster propulsion/vehicle impact study

    Weldon, Vincent / Dunn, Michael / Fink, Lawrence et al. | NTRS | 1988


    Booster propulsion/vehicle impact study, 2

    Johnson, P. / Satterthwaite, S. / Carson, C. et al. | NTRS | 1988


    Booster Propulsion/Vehicle Impact Study, 2

    P. Johnson / S. Satterthwaite / C. Carson et al. | NTIS | 1988


    Summary of booster propulsion/vehicle impact study results

    Weldon, Vincent A. / Fink, Lawrence E. / Phillips, Dwight U. | NTRS | 1988


    Summary of Booster Propulsion/Vehicle Impact Study Results

    V. A. Weldon / L. E. Fink / D. U. Phillips | NTIS | 1988