Design alternatives are considered for an autonomous three axis stabilized propulsion platform for use with space shuttle/Spacelab. An optimal configuration is presented, based on subsystem choices.


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    Title :

    Cost Analysis of the Propulsion of a Payload Transfer Module for Shuttle/Spacelab Applications on the Basis of Hybrid Rocket Engines Untersuchungen ueber die Kosten des Antriebs Eines Nutzlasttransfermoduls fuer Raumtransporter/Raumlaboratorium-Anwendungen Auf Basis von Zweistofftriebwerken


    Contributors:

    Publication date :

    1977


    Size :

    25 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English