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    In:  CASI
    Publication Date: 2019-06-27
    Description: Criteria for the design and development of turbines for rocket engines to meet specific performance, and installation requirements are summarized. The total design problem, and design elements are identified, and the current technology pertaining to these elements is described. Recommended practices for achieving a successful design are included.
    Keywords: PROPULSION SYSTEMS
    Type: NASA-SP-8110
    Format: application/pdf
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