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IV. Air-breathing propulsion systems for supersonic aircraftIn this part, the state of the art for several propulsion system components is reviewed, and some of the important factors which must be considered during the design of a supersonic propulsion system are pointed out. The discussion will be centered around the Mach number 3 cruise airplane of part III and the multimission airplane of part II.
Document ID
19670023745
Acquisition Source
Headquarters
Document Type
Other - Technical Report
Authors
Lowell E Hasel (Langley Research Center Hampton, Virginia, United States)
Willard E Foss, Jr. (Langley Research Center Hampton, Virginia, United States)
David N Bowditch (Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 3, 2013
Publication Date
October 1, 1960
Publication Information
Publication: Compilation of Papers Summarizing Some Recent NASA Research on Manned Military Aircraft
Publisher: National Aeronautics and Space Administration
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: National Meeting on the Future of Manned Military Aircraft
Location: San Diego, CA
Country: US
Start Date: August 1, 1960
End Date: August 3, 1960
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
67N33074
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Propulsion system
Air breathing engine
Supersonic aircraft
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