In order for the shuttle tug or interim upper stage (IUS) to capture all the missions in the current mission model for the tug and the IUS, an auxiliary or kick stage, using a solid propellant rocket motor, is required. Two solid propellant rocket motor technology concepts are described. One concept, called the 'advanced propulsion module' motor, is an 1800-kg, high-mass-fraction motor, which is single-burn and contains Class 2 propellent. The other concept, called the high energy upper stage restartable solid, is a two-burn (stop-restartable on command) motor which at present contains 1400 kg of Class 7 propellant. The details and status of the motor design and component and motor test results to date are presented, along with the schedule for future work. (Author)


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    Titel :

    Solid Rocket Technology Advancements for Space Tug and Ius Applications


    Beteiligte:
    W. Ascher (Autor:in) / R. L. Bailey (Autor:in) / J. W. Behm (Autor:in) / W. Gin (Autor:in)

    Erscheinungsdatum :

    1975


    Format / Umfang :

    28 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Solid rocket technology advancements for space tug and IUS applications

    Ascher, W. / Bailey, R. L. / Behm, J. W. et al. | NTRS | 1975




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