NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Toward scramjet aircraftThe possibility for civil, military, and remotely-piloted aviation above Mach 5 is discussed with reference to the scramjet. Actively cooled aircraft structures of low weight are described, together with jet nozzle design and combustion parameters. The scramjet is seen as operating alone or in tandem with ramjet propulsion, which would power an aircraft up to scramjet speeds. Attention is given to the specific impulse of the scramjet engine, with hydrogen as the primary fuel. Applications include: advanced reconnaissance and interceptor aircraft, strategic cruise (both aircraft and missiles), highly-maneuverable interceptor missiles, transports, aircraft-type launch vehicles, first stages for Space Shuttle launching craft, and single-stage-to-orbit vehicles. Research has focused on increasing the propulsion power of the scramjet engine, while reducing drag on the accompanying airframe.
Document ID
19780039512
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Jones, R. A.
(NASA Langley Research Center Hampton, VA, United States)
Huber, P. W.
(NASA Langley Research Center Hypersonic Propulsion Branch, Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
February 1, 1978
Publication Information
Publication: Astronautics and Aeronautics
Volume: 16
Subject Category
Aircraft Design, Testing And Performance
Accession Number
78A23421
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available