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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
Timeline
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
Name: Zachary LaBry
Phone: (424) 277-5673
Email: zachary.labry@ata-e.com
Phone: (424) 277-5673
Email: zachary.labry@ata-e.com
Business Contact
Name: Joshua Davis
Phone: (858) 480-2028
Email: jdavis@ata-e.com
Phone: (858) 480-2028
Email: jdavis@ata-e.com
Research Institution
N/A
Abstract
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. *
