NASA has identified aerobraking as a potentially critical technology for the Space Exploration Initiative (SEI). The size of Mars aerobrakes may be beyond the capabilities of future launch vehicles to place them into orbit in one launch. On-orbit assembly using facilities and operations developed under the Space Station Freedom (SSF) Program represent one approach for realizing such large structures. the results of early testing in this subject can help influence the future evolution of the SSF. The objectives are to: (1) generate empirical data on operational procedures for on-orbit assembly of a large Mars aerobrake; (2) develop aerobrake design concepts; (3) identify critical issues and requirements associated with SSF utilization; and (4) to stimulate student participation in the SEI.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Mars Aerobrake Assembly Demonstration


    Beteiligte:
    J. M. Garvey (Autor:in)

    Erscheinungsdatum :

    1991


    Format / Umfang :

    37 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Mars aerobrake assembly demonstration

    Garvey, John M. | NTRS | 1991


    Mars aerobrake assembly demonstration

    GARVEY, JOHN / LEE, GORDON / FILATOVS, JURI | AIAA | 1990


    Mars aerobrake assembly simulation

    FILATOVS, G. / LEE, GORDON / GARVEY, JOHN | AIAA | 1992


    Mars Optimal Aerobrake Maneuver Estimation

    Sarli, Bruno V. / Farres, Ariadna / Folta, David C. | NTRS | 2018


    Mars Optimal Aerobrake Maneuver Estimation

    Sarli, Bruno / Farres, Ariadna / Folta, David | NTRS | 2018