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Modeling and Simulation of the Stability of ORSC Main Combustion Chambers

Award Information

Agency:
Department of Defense
Branch:
Air Force
Award ID:
77053
Program Year/Program:
2008 / STTR
Agency Tracking Number:
F064-005-0078
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
IN Space, L.L.C.
3495 Kent Avenue Suite G100 West Lafayette, IN -
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 2008
Title: Modeling and Simulation of the Stability of ORSC Main Combustion Chambers
Agency / Branch: DOD / USAF
Contract: FA9550-08-C-0033
Award Amount: $499,933.00
 

Abstract:

The potential for combustion instability has historically been a hindrance in developing rocket engines, and nearly always represents the major technical risk in engine developments. This proposal addresses innovative approaches toward prediction of liquid rocket engine combustion instability, as well as innovations in full-scale engine stability verification. Specific objectives are to demonstrate modern experimental diagnostics for measuring combustion stability margin in conjunction with a three-level predictive approach comprising classical linear modeling, moderate-fidelity computational fluid dynamics, and high-fidelity hybrid RANS/LES simulations. This companion experimental/computational/analytical approach provides coupling between the experimental results and analyses at multiple levels of validation enabling a validated predictive tool for fullscale analysis. An existing oxidizer-rich preburner rated at 3600 psia is used to generate warm oxidizer for the experimental study of real-scale ORSC main chamber injectors. The final objective is to perform a stability analysis for a notional 250,000 lbf engine and define a protocol for stability verification of the full-scale engine. The end goals are to provide a revolutionary stability prediction methodology for demonstration during the IHPRPT Hydrocarbon Boost Engine project, and to provide the US propulsion community with a stability analysis methodology that takes full advantage of modern tools and commercial software.

Principal Investigator:

William Anderson
Associate Professor
7654962658
wanderso@purdue.edu

Business Contact:

Benjamin Austin, Jr.
General Manager
7657752107
bjaustin@inspacellc.com
Small Business Information at Submission:

IN SPACE, L.L.C.
1220 Potter Drive Suite 100 West Lafayette, IN 47906

EIN/Tax ID: 061678762
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
Research Institution Information:
PURDUE UNIV.
Aeronautics and Astronautics
315 North Grant Street
West Lafayette, IN 47907
Contact: William Anderson
Contact Phone: (765) 496-2658
RI Type: Nonprofit college or university