USA flag logo/image

An Official Website of the United States Government

Efficient and Accurate Computational Framework for Injector Design and Analysis

Award Information

Agency:
National Aeronautics and Space Administration
Branch:
N/A
Award ID:
77551
Program Year/Program:
2007 / SBIR
Agency Tracking Number:
053802
Solicitation Year:
N/A
Solicitation Topic Code:
N/A
Solicitation Number:
N/A
Small Business Information
Combustion Research and Flow Technology,
6210 Kellers Church Road Pipersville, PA 18947-
View profile »
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No
 
Phase 2
Fiscal Year: 2007
Title: Efficient and Accurate Computational Framework for Injector Design and Analysis
Agency: NASA
Contract: NNM07AA19C
Award Amount: $599,897.00
 

Abstract:

The proposed effort addresses a current need for high fidelity simulation tools to support the design and analysis of combustion devices for the Constellation program and Exploration Mission that includes earth-to-orbit, upper stage, as well as in-space propulsion systems. Injector designs are a critical component of robust thrust chamber assembly designs since they impact combustion chamber instability and its transient response. Inadequate injector designs have been the cause of major failures during engine development of all earlier liquid rocket systems including the SSME; the root cause for this may be attributed to the use of relatively simple empirically based, one-dimensional tools in the design process that are incapable of identifying localized failures driven by three-dimensional geometry and physics effects. The proposed three-dimensional, CFD tool will focus on rigorous modeling of the mixing and combustion processes in cryogenic liquid-gas injectors that operate in the trans-critical and sub-critical regime and exhibit strong non-linear sensitivities to real fluid thermodynamics, as well as turbulent mixing effects. The advanced models developed will permit improved predictions of combustion chamber mean heat flux and localized peaks, as well as lay the foundation for predicting unsteady response of the injector and its coupling to the feed system dynamics.

Principal Investigator:

Ashvin L. Hosangadi
Principal Investigator
2157661520
hosangad@craft-tech.com

Business Contact:

Paula A. Schachter
Business Official
2157661520
schachte@craft-tech.com
Small Business Information at Submission:

Combustion Research and Flow Technology
6210 Kellers Church Road Pipersville, PA 18947

EIN/Tax ID: 232759059
DUNS: N/A
Number of Employees:
Woman-Owned: No
Minority-Owned: No
HUBZone-Owned: No