The Orbiter Environmental Control and Life Support System (ECLSS) provides the functions of atmosphere revitalization, crew life support, active thermal conditioning, and airlock support for EVA and docking activities. The ECLSS must satisfy the requirements of orbital missions with four to ten crewmembers and mission duration of a few hours to 30 days and the requirements associated with an atmospheric horizontal flight test program and ferry flight missions. The ECLSS development plan utilizes an ECLSS ground test article and thermal/vacuum testing to support the first horizontal flight test at the end of 1976. The ground testing and horizontal flight test program certify the Orbiter ECLSS for the first orbital flight in early 1978.


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    Titel :

    Space Shuttle Orbiter ECLSS.


    Beteiligte:
    Stoll, O. T. (Autor:in) / Laubach, G. E. (Autor:in) / Gibb, J. W. (Autor:in)

    Kongress:

    Intersociety Conference on Environmental Systems ; 1973 ; San Diego, CA, US


    Erscheinungsdatum :

    1973-07-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Orbiter ECLSS support of shuttle payloads

    Jaax, J. / Morris, D. / Prince, R. | Tema Archiv | 1974


    Orbiter ECLSS support of Shuttle payloads

    Jaax, J. R. / Morris, D. W. / Prince, R. N. | NTRS | 1974



    Space Shuttle Environmental and Life Support System (ECLSS)

    Swider, Joseph E. / Galluccio, Richard | SAE Technical Papers | 1982


    Maintainability and Maintenance Approach to Orbiter ECLSS Design

    Linsday, T. H. | SAE Technical Papers | 1974