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Liquid propellant gas generatorsThe design of gas generators intended to provide hot gases for turbine drive is discussed. Emphasis is placed on the design and operation of bipropellant gas generators because of their wider use. Problems and limitations involved in turbine operation due to temperature effects are analyzed. Methods of temperature control of gas turbines and combustion products are examined. Drawings of critical sections of gas turbines to show their operation and areas of stress are included.
Document ID
19730018978
Document Type
Special Publication (SP)
Date Acquired
September 2, 2013
Publication Date
March 1, 1972
Subject Category
PROPULSION SYSTEMS
Report/Patent Number
NASA-SP-8081
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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NameType 19730018978.pdf STI