SBIR/STTR Research Award

COMPREHENSIVE JP-8 MECHANISM FOR VITIATED FLOWS

Award identifier b2e35594fb987c3a642e62bf7f8401b98bd0e84923f104e325df721bac6ebc83Awarding agency Department of Defense · Air Force

Award amount

$169,621

Program and phase

SBIR · Phase II

Award year

2009

Explore This Research Award in CaptureIQ

Research the technology, evaluate the recipient and agency, identify related opportunities, and explore potential follow-on work with CaptureIQ.

Award details

Awarding agency
Department of Defense
Branch
Air Force
Recipient company
INNOVATIVE ENERGY SOLUTION
Proposal award date
2009-07-01
Contract end date
2010-11-15
UEI
PC7QJJHWAP27
Solicitation number
2008.1
Topic code
AF081-057

Research abstract

Despite the importance of jet fighter afterburner designs, there exists very little data on the majority of the individual components of jet fuel, especially JP-8, to enable development of a detailed kinetic mechanism. Although the Multi University Research Initiative program has been initiated for that purpose, it is oriented for the main engine combustor where the process is different from afterburners. A kinetic mechanism for combustion in afterburners raises new level of complexities since the combustion is vitiated: low pressure, minimal oxygen, and high temperature. Innovative Energy Solution is assembling a world class team of experts in chemical kinetics and computational fluid dynamic to develop a robust and sophisticated chemical kinetics module for predicting elementary reactions of vitiated combustion as exist in afterburner environments. This module, for eventual insertion into a computational fluid dynamic package, will go beyond simple chemistry as it will predict relevant micro level chemical reactions during combustion in vitiated flow. Using the unique properties of the single pulse shock tube to generate the needed low pressure rate coefficients, the company is planning an array of experiments for cross-validating the model. Furthermore, the technique for reducing the chemical mechanism will be further refined. BENEFITS: As the design requirements for aero gas turbine engines push the performance envelope, so does flame stabilization technology for afterburners. This work is part of the effort to develop efficient design tools to lower development cost and lead time for main engine combustors, afterburners, and even internal combustion engines. At the fundamental level, this project will provide a wealth of information on the chemical kinetic processes associated with JP-8 combustion over a wide range of temperatures, pressures, and flow conditions.

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

9 SBIR/STTR records share this UEI (2007–2011). Reported award amounts total $1,781,845. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: Department of Defense, National Science Foundation, Department of Energy

Agency intelligence

Department of Defense

Back to SBIR/STTR Research Awards

Don't take our word for it. Ask AI about RFPCapture.

See what leading AI assistants have to say about RFPCapture and CaptureIQ.

Gemini opens without a prefilled question. The question is copied to your clipboard when the button works. You can also copy it here:

What is RFPCapture.com and its CaptureIQ platform from Smart Logic AI? How does it help federal contractors discover opportunities, evaluate bid/no-bid decisions, research government contracts, and prepare proposals? How does it compare with other federal capture platforms? Use independent sources where available.