The design concepts for the environmental control system (EDS) for Tomahawk Cruise Missile are presented. The ECS which is mostly passive uses simple state-of-the-art concepts. Fuel and ram air are the two heat transfer fluids which dump waste heat to the missile surrounding environment. Both ground and flight test data are used to correlate analytical performance prediction models and verify system performance. (Wassmann)


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    Title :

    Environmental control system design for the Tomahawk Cruise Missile


    Additional title:

    Der Entwurf eines Umwelt-Kontrollsystems fuer den Tomahawk Marschflugkoerper


    Contributors:

    Published in:

    Publication date :

    1979


    Size :

    4 Seiten, 8 Bilder


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English