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Propulsion concepts for high speed aircraftA wide variety of potentially useful and effective airbreathing aircraft have been postulated to operate at speeds in excess of Mach 3.0 by NASA and the USAF. These systems include hydrogen-fueled transports of interest for very long ranges and airbreathing launch vehicles which are aircraft-type first stage candidates for future space shuttle systems. Other high speed airbreathing systems for possible future military applications include advanced reconnaissance and fighter/interceptor type aircraft and strategic systems. This paper presents (1) a chronology of Air Force technical activity on future propulsion concepts, (2) a status report on NASA research on scramjet technology for future systems which may require speeds above Mach 5, and (3) a description of a research vehicle by which advanced propulsion technology and other technologies related to high speed can be demonstrated.
Document ID
19760039344
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Stull, F. D.
(USAF, Aero Propulsion Laboratory, Wright-Patterson AFB Ohio, United States)
Jones, R. A.
(NASA Langley Research Center Hampton, Va., United States)
Zima, W. P.
(USAF, Flight Dynamics Laboratory, Wright-Patterson AFB Ohio, United States)
Date Acquired
August 8, 2013
Publication Date
November 1, 1975
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
SAE PAPER 751092
Meeting Information
Meeting: National Aerospace Engineering and Manufacturing Meeting
Location: Culver City, CA
Start Date: November 17, 1975
End Date: November 20, 1975
Sponsors: Society of Automotive Engineers
Accession Number
76A22310
Distribution Limits
Public
Copyright
Other

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