A derivative of the Apollo Lunar Module is being developed to support the operation of a manned, earth orbiting solar observatory. Its thermal control and life support systems demonstrate how previously developed technology and hardware are satisfying mission requirements which differ significantly from those for which the vehicle was originally designed.Thermal control is accomplished by active and passive means. The active portion of the system employs liquid heat transport and rejection networks. Insulation systems, thermal coatings, and conductive couplings are used as much as is practical to minimize the effects on the vehicle of variations in the external thermal environment. The Apollo Lunar Module life support system has been extensively modified to permit both shirtsleeve and extravehicular crew activities.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Lunar Module Thermal Control and Life Support Systems for Apollo Applications


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Aeronautic and Space Engineering and Manufacturing Meeting ; 1969



    Erscheinungsdatum :

    01.02.1969




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Apollo Lunar Module control system

    Grossman, R.L. / Hagerman, R.H. / Williams, O.S. | Engineering Index Backfile | 1968


    Apollo Lunar Module Propulsion Systems Overview

    Interbartolo, Michael | NTRS | 2009


    The Apollo Lunar Module

    Ford, T.E. | Emerald Group Publishing | 1969