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Experience with low cost jet enginesA summary is given of the results of a NASA program for reducing the cost of turbojet and turbofan engines. The design, construction, and testing of a simple turbojet, designed for use in missiles, is described. Low cost axial stage fabrication, the design of a fan jet engine suitable for propulsion of light aircraft, and application of such engines to provide higher flight speeds, are discussed.
Document ID
19720020166
Document Type
Conference Paper
Authors
Cummings, R. L. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
E-6985
NASA-TM-X-68085
Meeting Information
Meeting: Natl. Business Aircraft Meeting
Location: Wichita, KS
Country: United States
Start Date: March 15, 1972
End Date: March 17, 1972
Sponsors: Soc. of Automotive Engr.
Accession Number
72N27816
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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