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Hypersonic research engine integrated propulsion control.Integrated propulsion control system for ramjet Hypersonic Research Engine to operate at 3-8 Mach numbers
Document ID
19690054755
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Colwill, T.
Curran, W.
Stiglic, P.
Date Acquired
August 5, 2013
Publication Date
June 1, 1969
Publication Information
Publisher: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS,
Subject Category
Propulsion Systems
Report/Patent Number
AIAA PAPER 69-546
Report Number: AIAA PAPER 69-546
Meeting Information
Meeting: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS, PROPULSION JOINT SPECIALIST CONFERENCE
Location: COLORADO SPRINGS, COLO.
Start Date: June 9, 1969
End Date: June 13, 1969
Sponsors: AMERICAN INST. OF AERONAUTICS AND ASTRONAUTICS
Accession Number
69A32744
Distribution Limits
Public
Copyright
Other

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