The Hermes crew escape module (CEM) is discussed. The CEM is a leakproof volume containing the cockpit and workstation in a front part designed from aerodynamic and ergonomic considerations, closed at the rear by a bulkhead. The floor is designed to sustain impact loads, leading to the choice of titanium for the cabin. Communication between the cabin and the cargo bay is assured by a tunnel closed by a hatch when insulation of the crew in the cabin is needed. The CEM can be ejected at any stage of the flight, from prelaunch to landing. The CEM can withstand a 24hr delay in recovery, e.g., in case of ditching in the ocean.


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    Title :

    Hermes Escape System


    Contributors:
    J. Colrat (author) / H. P. Nguyen (author) / H. Hirsch (author)

    Publication date :

    1988


    Size :

    6 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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