SBIR/STTR Research Award

High-Performance Reticulated SiC Foam Injector for Liquid Rocket Engines

Award identifier aa498488f4d7de9d5556ad576f943f840d7fbfe58ebea6f2802e4ad6a8bdebf1Awarding agency Department of Defense · Air Force

Award amount

$100,000

Program and phase

SBIR · Phase I

Award year

2003

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Hyper-Therm High-Temperature Composites
Proposal award date
Not reported
Contract end date
Not reported
UEI
WRLGUJSGKJG8
Solicitation number
Not reported
Topic code
Not reported

Research abstract

Hydrocarbon-based fuels are being considered for reusable rocket engines because of high propellant density and high thrust-to-weight. Current developments are focusing on staged combustion cycles utilizing oxygen-rich preburners with liquid-liquidinjection. A need exists for advanced injectors with high mixing efficiencies, improved combustion stability and reusability. Recent developments in porous reticulated ceramic foams offer promise to increase injector performance via improved mixingefficiencies and combustion stability; increase robustness and reliability via reduced vulnerability to particulate fouling and coking contamination of injector orifices; and decrease cost via eliminating the need for precision laser machining numeroussmall diameter orifice holes, thus greatly simplifying fabrication.The objective of this Phase I program is to demonstrate the feasibility of producing a reticulated SiC foam bipropellant injector assembly with improved performance and simplified fabrication over traditional designs that may suitable for booster-scale,hydrocarbon-based rocket engine application. Reticulated SiC foam specimens of various porosities and densities will be produced and experimentally evaluated to determine their respective liquid and gaseous pressure drop characteristics, dischargecoefficients and potential for use in an advanced propellant injector design. A prototype single-element SiC foam bipropellant injector assembly will be designed, fabricated and delivered to OSD for hot-fire ground test evaluation. Reticulated ceramic and refractory metal foams are an enabling class of materials which are suitable for a variety of extreme environment applications including chemical rocket propulsion injectors, hot gas and molten metal filters, catalyst supports andradiant burners. Ceramic foams are currently being used as a low-density core in high-rigidity ceramic composite sandwich structures and ultra-lightweight laser mirrors and optics.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

68 SBIR/STTR records share this UEI (1993–2013). Reported award amounts total $17,201,144. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Aeronautics and Space Administration, Department of Energy

Agency intelligence

Department of Defense

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