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Liquid rocket engine turbinesCriteria 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.
Document ID
19740026132
Acquisition Source
Legacy CDMS
Document Type
Special Publication (SP)
Date Acquired
September 3, 2013
Publication Date
January 1, 1974
Subject Category
Propulsion Systems
Report/Patent Number
NASA-SP-8110
Report Number: NASA-SP-8110
Accession Number
74N34245
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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