Multi-Phase Flow Analysis Tools for Solid Motor Applications

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$100,000.00
Award Year:
2008
Program:
STTR
Phase:
Phase I
Contract:
NNX08CD48P
Agency Tracking Number:
070188
Solicitation Year:
2007
Solicitation Topic Code:
T8.02
Solicitation Number:
n/a
Small Business Information
Tetra Research Corporation
420 Park Avenue West, Princeton, IL, 61356-1934
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
Y
Duns:
969308311
Principal Investigator:
Rex Chamberlain
Principal Investigator
(815) 872-0702
rex@tetraresearch.com
Business Contact:
Rex Chamberlain
Business Official
(815) 872-0702
rex@tetraresearch.com
Research Institution:
Mississippi State University
Not Available
Engineering Research Center
Mississippi State, MS, 39762
(662) 325-4586
Domestic nonprofit research organization
Abstract
The challenges of designing, developing, and fielding man-rated propulsion systems continue to increase as NASA's Vision for Space Exploration Program moves beyond the Space Shuttle and RSRM. The number and type of different propulsion elements required are significant, and predicting internal solid motor behavior and characteristics and assessing external environments due to plume impingement on vehicle structures is a top priority. Solid motors do not require pre-start thermal conditioning but can be throttled by grain shape and pintle design, and thus the analysis tools must be flexible and prepared to meet the appropriate simulation readiness level. Our proposed innovation will enhance existing engineering software by combining new flow solution methodologies with appropriate boundary conditions to create a novel toolset for complex multi-phase solid rocket analyses. The innovation will be based on the LOCI/CHEM multi-physics analysis package and will utilize new LOCI features, new multi-phase flow models, and theoretical and phenomenological boundary conditions to create a unique software tool for solid propellant burning, particle breakup, surface erosion, and environment characterization for next generation solid motors. Our research products will provide NASA with the important capability to simultaneously analyze solid propellant combustion, heat transfer, and nozzle erosion within a single numerical framework.

* information listed above is at the time of submission.

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