Continuous Detonation Rocket and Air Breathing Engines

Award Information
Agency:
Department of Defense
Branch
Defense Advanced Research Projects Agency
Amount:
$98,937.00
Award Year:
2008
Program:
SBIR
Phase:
Phase I
Contract:
W31P4Q-09-C-0197
Award Id:
86356
Agency Tracking Number:
08SB2-0891
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
2629 Townsgate Road, Suite 105, Westlake Village, CA, 91361
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
005100560
Principal Investigator:
RamakanthMunipalli
Sr. Computational Physicist
(805) 371-7500
mrk@hypercomp.net
Business Contact:
VijayaShankar
Vice-President
(805) 371-7556
vshankar@hypercomp.net
Research Institute:
n/a
Abstract
We propose here a systematic sequence of advancements which can lead to the efficient and reliable operation of continuous detonation engines. The advancements sought will pertain to fuel injection, initiation and sustenance of detonation waves and the geometrical design of detonation channels and nozzles. A scalability study will be performed to assess the feasibility of the detonation engine at larger thrust levels and design alternatives needed at higher thrust levels will be explored. Phase-I research will rely upon analytical and computational models, and a test program is planned at the University of Texas at Arlington (UTA) for a potential second phase of this project. Ample prior experience on all these fronts is available with the proposing team of HyPerComp and UTA.

* information listed above is at the time of submission.

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