Pulse Detonation Engines Cycle Analysis and Performance Prediction Code

Award Information
Agency:
Department of Defense
Branch
Navy
Amount:
$303,927.00
Award Year:
2008
Program:
SBIR
Phase:
Phase II
Contract:
N00014-08-C-0548
Award Id:
82646
Agency Tracking Number:
N071-069-1222
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
340 SENTINEL OAK DRIVE, DAYTON, OH, 45458
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
966649048
Principal Investigator:
Mohammed Mawid
Senior Scientist
(937) 291-3800
mohammed.mawid@engineeringrac.com
Business Contact:
Mohammed Mawid
Technical Director
(937) 291-3800
mohammed.mawid@engineeringrac.com
Research Institution:
n/a
Abstract
An integrated Pulse Detonation Engine (PDE)and Airframe Transient Cycle Analysis and Airframe Performance (PDE-CAASP) code is proposed for development based upon the successful development of a PDE Transient Cycle Analysis Code during Phase-I. The Integrated PDE/Airframe code will include flight dynamics, aerodynamics, weight & Stucture, mission, and PDE propulsion models to set and predict the integrated PDE/Airframe performance for selected warefighting missions. The new PDE-CAASP code will be very efficient, cost-effective, and rapid to provide estimates of the potential PDE-powerd air vehicles over existing ramjet and turbine-powered flight vehicles and as such the PDE-CAASP code will be very unique and represents a new enabling technology for the US Navy.

* information listed above is at the time of submission.

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