SBIR/STTR Research Award

Fire Suppressant Transport Modeling

Award identifier 17e812b93b57ab3ce66e5ee55b97f30f0027ca7040460e36b2752437642e3dc8Awarding agency Department of Defense · Air Force

Award amount

$749,988

Program and phase

SBIR · Phase II

Award year

2014

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Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
ADA TECHNOLOGIES LLC
Proposal award date
2014-06-24
Contract end date
2016-06-23
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 fire testing can be mitigated by modeling. In this Phase II project, ADA Technologies is partnering with Fire Science NM and SURVICE Engineering to develop, validate and implement 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, such as the dispersion of fire suppressant. The Phase I preliminary model demonstrated the required speed and accuracy. In Phase II, the code will be further streamlined and thoroughly validated against full-scale test data. Finally, the code will be converted to a module and integrated into the FPM (Fire Prediction Model) platform for use by the DoD survivability community. 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 for dry bay and engine nacelles 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. DOD markets include a variety of new and retrofit applications linked under the joint aircraft survivability program. Beyond military aircraft, commercial aircraft is another natural fit for the code, as airframers are facing the same issue for engine nacelle and APU protection. Finally, weight and cost optimization of fire suppression systems of other, non-aerospace 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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