COMBUSTION SCIENCE & ENGINEERING, INC. — Department of Defense SBIR Phase I: AF191-068

COMBUSTION SCIENCE & ENGINEERING, INC. — SBIR Phase I award from Department of Defense.

Phase I SBIR feasibility signal

  • Phase I awards fund proof-of-concept work. For capture teams, they mark early interest from Department of Defense in a technical approach.
  • Watch for Phase II follow-ons from the same firm/topic family — that conversion path is where budgets and transition pressure rise.
  • Obligated amount $149,971. Cross-check similar awards in the same agency and technology tags for going-rate context.
  • Topic code AF191-068 links this award to a solicitation family — search the same topic stem for incumbents and recompete timing.

Informational capture context from public federal data — not legal or bid advice.

Amount
$149,971
Agency
Department of Defense · Air Force
Program / Phase
SBIR · Phase I
Topic
AF191-068
Solicitation
19.1
NAICS
—
Place of performance
MD
Period
2019-08-20 → 2020-08-20

Description

The objective of this project is to improve the state-of-the-art detailed chemical kinetic models for rocket fuels using relevant experimental data at liquid rocket engine (LRE) conditions. This improved kinetic model will be used to develop reduced kinetic models that can be used for computational fluid dynamics (CFD) simulations of LRE for design purpose. To achieve these goals, Combustion Science & Engineering, Inc. (CSE) will collaborate with Stanford University to evaluate the performance of the existing models and identify the reactions or reaction subsets that need to be improved to reduce the uncertainty of the model predictions at LRE relevant conditions. Preliminary experiments will be conducted in Phase I to acquire reaction rate data in order to improve the model performance. Moreover, CSE will develop methodologies to develop reduced kinetic models for CFD simulations of LRE systems. The reduced kinetic models will be evaluated for computational efficiency and accuracy by simulating canonical test problems using standalone linear eddy model.