The conceptual design studies of a Block 2 Solid Rocket Motor (SRM) require the elimination of asbestos-filled insulation and was open to alternate designs, such as case changes, different propellants, modified burn rate - to improve reliability and performance. Limitations were placed on SRM changes such that the outside geometry should not impact the physical interfaces with other Space Shuttle elements and should have minimum changes to the aerodynamic and dynamic characteristics of the Space Shuttle vehicle. Previous Space Shuttle SRM experience was assessed and new design concepts combined to define a valid approach to assured flight success and economic operation of the STS. Trade studies, preliminary designs, analyses, plans, and cost estimates are documented.


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    Titel :

    Block 2 SRM (Solid Rocket Motor) Conceptual Design Studies. Volume 1, Book 1: Conceptual Design Package


    Beteiligte:
    B. Smith (Autor:in) / N. Williams (Autor:in) / J. Miller (Autor:in) / J. Ralston (Autor:in) / J. Richardson (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    275 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch