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Continuous Detonation Rocket and Air Breathing Engines

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: W31P4Q-09-C-0280
Agency Tracking Number: 08SB2-0896
Amount: $98,982.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: SB082-059
Solicitation Number: 2008.2
Timeline
Solicitation Year: 2008
Award Year: 2009
Award Start Date (Proposal Award Date): 2009-02-17
Award End Date (Contract End Date): 2009-10-30
Small Business Information
1832 180th St. SE
Bothell, WA 98012
United States
DUNS: 086581902
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Jerry Berg
 Sr. Mechanical Engineer
 (425) 487-4020
 jerry.berg@systima.com
Business Contact
 Tom Prenzlow
Title: President
Phone: (425) 487-4020
Email: tom.prenzlow@systima.com
Research Institution
N/A
Abstract

Proposal will develop and study feasibility of Continuous Detonation Rocket Engine (CDRE) systems for rocket and combined cycle engines. Systima Technologies, Inc., Geminus Technology Development, LLC and the University of Washington, Fluids and Propulsion Labs have detonation engine expertise and propose to develop a working CDRE computational model, design demonstration CDRE, and feasibility analysis of CDRE. This effort has full support of Pratt & Whitney’s active continuous detonation experience. Detonation engines should exhibit higher levels of performance with more efficient thermodynamic properties over conventional constant-pressure combustion systems. Study of unsteady combustion systems is key to addressing continued interest in advanced engines such as Rocket Based Combined Cycle (RBCC), Turbine Based Combined Cycle (TBCC) and Single Stage To Orbit (SSTO). This proposal is instrumental to advance this technology and assess potential advantages. Under similar conditions, detonation is more efficient combustion process over deflagration. This is evidenced by lower increases in entropy during detonation and its thermodynamic advantage. The challenge is applying detonation into propulsion. CDRE’s advantages over conventional detonation engines are simplicity and performance. The Systima-Geminus-University of Washington-Pratt & Whitney team proposes computational modeling, feasibility analysis, and an experimentation in parallel to advance CDRE technology and evaluate its potential.

* Information listed above is at the time of submission. *

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