NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
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
Acquisition Source
Legacy CDMS
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
Report Number: E-6985
Report Number: 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.

Related Records

There are no records associated with this record.
No Preview Available