STTR Phase I: Multi-Dimensional Hydrodynamic Stability Analysis Tool for Solid Rocket Motors

Award Information
Agency: National Science Foundation
Branch: N/A
Contract: 0611362
Agency Tracking Number: 0611362
Amount: $99,973.00
Phase: Phase I
Program: STTR
Awards Year: 2006
Solicitation Year: 2006
Solicitation Topic Code: CT
Solicitation Number: NSF 05-605
Small Business Information
1802 North Carson St, Carson City, NV, 89701
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Jonathan French
 (775) 882-1966
Business Contact
 Jonathan French
Phone: (775) 882-1966
Research Institution
 Univ of TN Space Inst
 Joseph Majdalani
 411 B H Goethert Parkway
Tullahoma, TN, 37388
 (931) 393-7280
 Nonprofit college or university
This Small Business Technology Transfer (STTR) Phase I project is to determine the feasibility of developing a hydrodynamic combustion stability analysis design tool for rockets, gas turbines, and large engines. As combustors are run at leaner mixture ratios to avoid NOx pollutant issues, vortex liquid rocket engines are designed with swirling flows to cool engines, and solid rocket motors are built with longer L/D ratios, combustion stability issues associated with rotating flows become significant concerns. In this work analytic models applied to simple geometries will be transferred into a general 3D capable stability tool. For this initial endeavor, the focus is on developing a hydrodynamic stability tool for the solid rocket motor industry. Currently, many large solid rocket motors exhibit hydrodynamic stability problems, including the Shuttle RSRM, Titan, and the Ariane V. By avoiding stability issues in the design process, this tool has the potential to not only save on revenue and loss in momentum, but also prevent developmental programs from being cancelled due to design problems late in the process.

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

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