SBIR/STTR Research Award

Fire Suppressant Transport Modeling

Award identifier b4541e1697ff1187780b85cd692ab6eded6022321dcd7b979f7b98a475349335Awarding agency Department of Defense · Air Force

Award amount

$143,982

Program and phase

SBIR · Phase I

Award year

2012

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ADA TECHNOLOGIES LLC
Proposal award date
2012-08-16
Contract end date
Not reported
UEI
NQEGVMEYYRT9
Solicitation number
2012.1
Topic code
AF121-197

Research abstract

ABSTRACT: Fires initiating in engine nacelles and dry bays are the most common causes of loss of aircraft. However, since the Montreal Protocol restricting the production of Halons, a replacement has not yet been accepted by the aircraft survivability community despite numerous testing programs. The costs and limitations of designing new systems based primarily on live testing can be mitigated by modeling. ADA Technologies is partnering with ARA to propose the development and preliminary validation of a fast-running, physics-based, computational fluid dynamics (CFD) code for mapping the concentration of clean agent fire suppressants in obstructed environments such as dry bays. At the core of the simplified approach is the focus on the low-Mach number equations, describing phenomenon happening in the subsonic regime. This is appropriate for dispersion of fire suppressant exiting nozzles at velocities smaller than Mach 0.2. Our approach contains three steps: acquisition of relevant experimental data in our lab, modeling of the experiment with a fast code on a PC, and comparison of the results with the output from a comprehensive CFD code running on a computer cluster. As a result, the product of this project will be an experimentally validated code. BENEFIT: A fast-running CFD code modeling the dispersion of Halon replacements, also known as clean agents, would allow optimization of new fire suppression designs by minimizing the amount of suppressant to be carried on-board an aircraft while ensuring satisfactory extinguishment performance. Limiting weight is always a primary concern in aircraft applications. Finding an effective and environmentally friendly replacement for Halon 1301 in dry bay systems would be greatly aided by such a validated CFD code. This code would be applicable to a variety of fire suppression applications looking for optimized Halon replacement systems. Beyond military aircraft, commercial aircraft is a natural fit for the code, as the FAA is struggling with the same issue. Outside aerospace markets, weight and cost optimization of the protection of other obstructed volumes is another commercialization opportunity. For examples, light armored vehicles in the DOD market and server rooms in the commercial sector represent promising business prospects for the future code.

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

274 SBIR/STTR records share this UEI (1985–2025). Reported award amounts total $89,993,036. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

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

Agency intelligence

Department of Defense

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