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Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- Nirvana Technologies, Inc.
- Proposal award date
- 2021-05-01
- Contract end date
- 2022-02-01
- UEI
- RBBAZ7GJH2M5
- Solicitation number
- 19.2
- Topic code
- AF192-007
Research abstract
In order to develop and validate combustion kinetic models, fundamental combustion chemistry properties such as ignition delays are critical. We propose to design and develop a fully characterized, standardized, compact, diaphragmless and automated shock tube facility integrated with optical sensors with operating protocol. The proposed shock tube facility is designed for operation with low operating cost and allow field deployment. The proposed shock tube facility is expect to achieve the following features: (1) diaphragmless to remove the highly experience dependent conventional diaphragm for shock generation; (2) the shock tube has “Uâ€Â shape arrangement therefore it is compact and its overall length is only approximately 3 m; (3) the operational conditions will be standardized and fully characterized before deployment therefore the experimental uncertainty and error induced by non-expert operation could be significantly minimized. The shock tube facility will be integrated with optical sensors to achieve fully automated data collection including autoingition delays and speciation histories.
Technology keywords
Not reported
Other awards by this recipient
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Awards with the same topic code
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Research funding history
2 SBIR/STTR records share this UEI (2020–2021). Reported award amounts total $274,406. Reported amounts are not federal obligations.
Phases: Phase I
Agencies: Department of Defense, National Aeronautics and Space Administration
Agency intelligence
Department of Defense
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