A 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. (Author)
Experience with Low Cost Jet Engines
1972
20 pages
Report
No indication
English
Experience with low cost jet engines.
NTRS | 1972
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