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a case for basic rotating detonation engine researchA brief review is provided covering the benefits to air breathing and chemical rocket propulsion found from pressure gain combustion in general, and rotating detonation in particular. Challenges are also identified.
Document ID
20170001670
Document Type
Presentation
Authors
Paxson, Daniel E.
(NASA Glenn Research Center Cleveland, OH United States)
Date Acquired
February 21, 2017
Publication Date
May 26, 2016
Subject Category
Aircraft Propulsion and Power
Report/Patent Number
GRC-E-DAA-TN32567
Meeting Information
DARPA RDE Stakeholders Day(Arlington, VA)
Funding Number(s)
WBS: WBS 109492.02.03.02.30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
propulsion
detonation
combustion

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