SBIR-STTR Award

Establishing a Practical and Accurate Combustion Mechanism for JP-10
Award last edited on: 4/30/2019

Sponsored Program
STTR
Awarding Agency
DOD : Navy
Total Award Amount
$69,921
Award Phase
1
Solicitation Topic Code
N09-T011
Principal Investigator
Sivaram P Gogineni

Company Information

Spectral Energies LLC

4065 Executive Drive
Beavercreek, OH 45430
   (937) 902-6546
   contact@spectralenergies.com
   www.spectralenergies.com

Research Institution

University of Massachusetts - Amherst

Phase I

Contract Number: N68335-09-C-0369
Start Date: 7/16/2009    Completed: 2/16/2010
Phase I year
2009
Phase I Amount
$69,921
JP-10 is a single-compound C10H16 fuel that is the principal air-breathing missile fuel used in the U.S. at present. We propose that its effective use can be advanced by modeling its chemistry and combustion physics, testing these predictions against laboratory and full-scale experiments, and then using the information for computational design and operations. In this Phase I research project, we propose to develop the JP-10 decomposition subset of a full combustion mechanism of elementary reactions, based on analogies with known reactions and from computed predictions of kinetics, thermochemistry, and transport properties. Scientists at Spectral Energies, LLC will work with collaborators and the Navy to determine appropriate validation experiments in an aerosol shock tube to study the relevant high temperature decomposition products of JP-10 over a range of temperatures, pressures, and equivalence ratios relevant to ramjet and scramjet propulsion. Spectral Energies will also initiate simulations using Chemkin-based combustion models for comparison with experimental data from the literature. These results would set the basis for Phase II experimental tests of the reaction set, improvements to it, and mechanism reduction for efficient combustor modeling. Time dependent measurements of temperature, the hydroxyl radical, and water decomposition products will also be used during the Phase II to validate predictions of ignition and flame propagation.

Benefit:
This work will enable model-based optimization of ramjet and scramjet engine design, leading to reduced development time, reduced cost, more compact hardware, and improved reliability. The model for chemical kinetics, thermochemistry, and transport properties that results from this program can be incorporated into new or existing DoD or NASA programs where JP-10 is used as a fuel. In addition, the aerospace industry can use the data gained from this research for applications that require high energy density, such as the emerging UAV market and propulsion for space access.

Keywords:
Chemical Kinetics, Chemical Kinetics, Transport Properties, decomposition products, JP-10

Phase II

Contract Number: ----------
Start Date: 00/00/00    Completed: 00/00/00
Phase II year
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Phase II Amount
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