SBIR/STTR Research Award
The Chemical and Physical Mechanism Processes of Al-Al2O3 within the Accelerating Flow-Field of Solid Rocket Motors (SRM)
Award amount
$990,960Program and phase
SBIR · Phase IIAward year
2017Award details
- Awarding agency
- Department of Defense
- Branch
- Army
- Recipient company
- PHYSICAL SCIENCES INC.
- Proposal award date
- 2017-08-15
- Contract end date
- 2019-08-15
- UEI
- RMG1AZ1ZH8Q7
- Solicitation number
- 2016.0
- Topic code
- MDA11-029
Research abstract
Physical Sciences Inc. proposes to measure the Al-Al2O3 particle behavior in the supersonic plume of solid rocket motors (SRM) to ensure the development of a robust and accurate physics based exhaust plume flow field and signature prediction capability.An existing highly instrumented SRM ground based test facility will be used to conduct experimental measurements enabling the calibration and parameterization of motor performance and plume signature models. The targeted experimental measurements will acquire mechanistic understanding of the Al-Al2O3 particle distribution within the motors plume flow field and further the development of a comprehensive suite of sub-models that capture the particulate processes.
Technology keywords
Not reported
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
- Experimental and Modeling Investigation of Particle Interaction in SRM Exhaust Flows
- A Toolkit for Enhanced Particulate Simulation (EPSilon Toolkit) in Plume
- A Toolkit for Enhanced Particulate Simulation (EPSilon Toolkit) in Plume
- Experimental and Modeling Investigation of Particle Interaction in SRM Exhaust Flows
- Advanced Particulate Sub-Models for Rocket Motor Exhaust Plumes