This program will focus on the integration of all functional disciplines of the design, manufacturing, materials, fabrication and producibility to define and demonstrate a highly reliable, easily maintained, low cost liquid methane turbopump as a component for the STBE (Space Transportation Booster Engine) using the STME (main engine) oxygen turbopump. A cost model is to be developed to predict the recurring cost of production hardware and operations. A prime objective of the program is to design the liquid methane turbopump to be used in common with a LH2 turbopump optimized for the STME. Time phasing of the effort is presented and interrelationship of the tasks is defined. Major subcontractors are identified and their roles in the program are described.


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    Title :

    Advanced Launch System propulsion focused technology liquid methane turbopump technical implementation plan


    Contributors:
    Csomor, A. (author) / Nielson, C. E. (author)

    Publication date :

    1989-05-25


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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