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    Space shuttle hypergolic bipropellant RCS engine design study, Bell model 8701 (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: A research program was conducted to define the level of the current technology base for reaction control system rocket engines suitable for space shuttle applications. The project consisted of engine analyses, design, fabrication, and tests. The specific objectives are: (1) extrapolating current engine design experience to design of an RCS engine with required safety, reliability, performance, and operational capability, (2) demonstration of multiple reuse capability, and (3) identification of current design and technology deficiencies and critical areas for future effort.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-CR-134336 , REPT-8701-910041
    Format: application/pdf
    Location Call Number Expected Availability
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