Confined Recirculation Combustion Afterburner

Award Information
Agency:
Department of Defense
Branch
Air Force
Amount:
$749,694.00
Award Year:
2005
Program:
SBIR
Phase:
Phase II
Contract:
FA8650-05-C-2520
Award Id:
67702
Agency Tracking Number:
F041-188-0187
Solicitation Year:
n/a
Solicitation Topic Code:
n/a
Solicitation Number:
n/a
Small Business Information
880 Jupiter Park Drive, Suite 8, Jupiter, FL, 33458
Hubzone Owned:
N
Minority Owned:
N
Woman Owned:
N
Duns:
017391348
Principal Investigator:
DanHaid
Combustion Engineer
(561) 741-3441
danhaid@spiritech.cc
Business Contact:
RichDeFrancesco
President
(561) 741-3441
defran@spiritech.cc
Research Institute:
n/a
Abstract
The future of manned and unmanned vehicles requires significant improvements in engine thrust-to-weight ratio, efficiency, length, and cost. These improvements may be realized in the afterburner for supersonic missiles, Mach 8-10 strike/reconnaissance aircraft, and hypersonic vehicles operating with a Turbine Based Combined Cycle (TBCC). SPIRITECH Advanced Products, Inc. is proposing to increase the thrust -to-weight ratio of turbine engines with Confined Recirculation Combustion. Integrating this advancement into a compact, lightweight, robust, and highly efficient afterburner has the potential of reducing the overall length and corresponding hardware weight, enabling supersonic and hypersonic aircraft, and providing affordable, on-demand access to space with aircraft-like operations. The objectives of this Phase II program are to validate, through prototype testing, the combustion efficiency and operability of SPIRITECH's CRC afterburner design, including the effects of the upstream main combustor. These test results will be used to further validate/benchmark SPIRITECH's 3D CFD analytical model and apply it in the development of a final CRC afterburner concept.

* information listed above is at the time of submission.

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