SBIR/STTR Research Award

Injector Stability Screening Technique (ISST)

Award identifier 56598b2eaa1b1d2151797abc303af28b53e0f1aed235517c2c3b38130c9982c7Awarding agency Department of Defense · Air Force

Award amount

$746,528

Program and phase

SBIR · Phase II

Award year

2011

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
Orbital Technologies Corporation
Proposal award date
2011-03-25
Contract end date
Not reported
UEI
XESXD6N437K9
Solicitation number
2008.3
Topic code
AF083-112

Research abstract

ABSTRACT: ORBITEC proposes to demonstrate and validate a laboratory-scale experimental injector stability screening technique which will quantify injector element stability characteristics. The experimental approach promises to dramatically reduce development cost by utilizing a gaseous single element test facility which presents savings in hardware manufacturing, consumables, and test facility labor. The simple test facility will allow rapid stability characterization of multiple candidate injectors which will be unobtrusive to schedule requirements. The key cost and time savings will be fewer full-scale hardware configurations that must be manufactured which will in turn reduce the number of full-scale tests required for qualification. The Phase I effort evaluated a Russian pentad injector at full-scale and laboratory-scale conditions. Correlation between laboratory scale and full scale experimental data showed that both combustion devices operated without experiencing high frequency combustion instability. During Phase II, an available database for the injector will be utilized to ensure unstable operation which will be scaled up for engine testing. Laboratory-scale methods of providing similarity such as heating and reactant dilution will also be evaluated. The Phase II programs will set the necessary scaling requirements and produce plans for Phase III ORBITEC test facility implementation. BENEFIT: The end product of this overall research and validation effort will create an experimental test facility and scaling technique which will significantly decrease engine development time at a reduced cost. The scaling technique will have application to virtually all high pressure liquid rocket engine development programs and existing engine upgrades for the Air Force, Navy, MDA, NASA and their contractors as well as commercial satellite launch companies. Development may reveal application to the screech phenomenon in air-breathing engines which will significantly open the commercial aircraft sector.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

216 SBIR/STTR records share this UEI (1989–2014). Reported award amounts total $56,646,148. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense, Department of Agriculture, Department of Health and Human Services, National Science Foundation, Department of Energy

Agency intelligence

Department of Defense

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