Scramjet/Ramjet Heat Exchanger Analysis Tool

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$99,989.00
Award Year:
2005
Program:
SBIR
Phase:
Phase I
Contract:
FA8650-05-M-2578
Agency Tracking Number:
F051-192-0751
Solicitation Year:
2005
Solicitation Topic Code:
AF05-192
Solicitation Number:
2005.1
Small Business Information
SPIRITECH ADVANCED PRODUCTS, INC.
880 Jupiter Park Drive, Suite 8, Jupiter, FL, 33458
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
017391348
Principal Investigator:
Eric Gamble
Aero/Thermal Lead Engineer
(561) 741-3441
egamble@spiritech.cc
Business Contact:
Rich DeFrancesco
President
(561) 741-3441
defran@spiritech.cc
Research Institution:
n/a
Abstract
A ramjet/scramjet heat exchanger design and optimization tool is proposed for rapid analyses of complex thermal cooling systems. In the emerging field of high-speed aerospace, it is necessary that rapid modeling of complex thermal systems be accomplished to enable the trade studies required to optimize the design for weight, cost, and performance. To meet this need, SPIRITECH proposes the development of a ramjet/scramjet heat exchanger design and optimization tool that performs a thermal analysis of the heat exchanger, assesses its structural strength, and optimizes the heat exchanger design to minimize the cooling flow requirement and the heat exchanger weight. Options for the coolant fuel, including various jet fuels and endothermic additives, will be made available so that various fuels may be evaluated. In addition, options for various material properties will also be included. The Phase I effort will focus on developing the thermal and structural models as well as the optimization routine, resulting in a working code. This code will be packaged with a user-friendly interface to simplify its use for large trade studies. The Phase II effort will provide test data for code verification and will incorporate enhancements to improve accuracy and reduce run time.

* information listed above is at the time of submission.

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