Following the Space Shuttle Challenger accident, serious attention has turned to in-flight escape. Prior to the resumption of flight, a manual bailout system was qualified and installed. For the long term, a seated extraction system to expand the escape envelope is being investigated. This paper describes a 1987 study, conducted jointly by NASA/Johnson Space Center and Langley Research Center, to determine the feasibility of modifying the Space Shuttle Orbiters to incorporate the seated extraction system. Results of the study are positive, indicating retrofit opportunity and high probability of escape for early ascent, late entry, and even for uncontrolled flight such as the Challenger breakup. The system, as envisioned, can extract seven crewmembers within two seconds.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Shuttle seated extraction feasibility study


    Beteiligte:

    Kongress:

    Annual SAFE Symposium ; 1988 ; Las Vegas, NV, United States


    Erscheinungsdatum :

    1989-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Feasibility study of LITVC for shuttle SRB

    Martin, C. L. / Powers, L. B. | NTRS | 1981


    Feasibility Study of LITVC for Shuttle SRB

    C. L. Martin / L. B. Powers | NTIS | 1981


    FRAME STRUCTURE OF SEATED HANDCART AND SEATED HANDCART

    YOSHIDA KOMEI | Europäisches Patentamt | 2016

    Freier Zugriff