Detailed designs were made for three earth orbital propulsion systems; (1) the space shuttle (integrated) OMS/RCS, (2) the space shuttle (dedicated) OMS (LO2), and (3) the space tug. The preferred designs from the integrated OMS/RCS were used as the basis for the flight test article design. A plan was prepared that outlines the steps, cost, and schedule required to complete the development of the prototype DSL tank and feedline (LH2 and LO2) systems. Ground testing of a subscale model using LH2 verified the expulsion characteristics of the preferred DSL designs. (Author)


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    Title :

    Acquisition/Expulsion System for Earth Orbital Propulsion System Study. Volume 2: Cryogenic Design


    Publication date :

    1973


    Size :

    307 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English