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Shock-Tube-Validated, Versatile Kinetic Mechanism Reduction Framework for Mixed Hydrocarbon-Based Rocket Fuels

Award Information
Agency: Department of Defense
Branch: Air Force
Contract: FA9300-22-C-6032
Agency Tracking Number: F191-068-0059
Amount: $749,984.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: AF191-068
Solicitation Number: 19.1
Solicitation Year: 2019
Award Year: 2022
Award Start Date (Proposal Award Date): 2022-09-19
Award End Date (Contract End Date): 2024-12-20
Small Business Information
13290 Evening Creek Drive South
San Diego, CA 92128-4695
United States
DUNS: 133709001
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Zachary LaBry
 (424) 277-5673
Business Contact
 Joshua Davis
Phone: (858) 480-2028
Research Institution

Accurate characterization of liquid rocket engines (LREs) requires chemical modeling capable of predicting key quantities such as heat release rate, pressure rise, flow-combustion coupling, and pollutant formation. Reduced chemical mechanisms attempt to a

* Information listed above is at the time of submission. *

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