SBIR/STTR Research Award
Predicting the Flow Interactions of Modular Liquid Rocket Engine Thrust Chambers
Award amount
$728,858Program and phase
SBIR · Phase IIAward year
2017Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- WASK Engineering, Inc.
- Proposal award date
- 2017-01-18
- Contract end date
- 2019-02-19
- UEI
- MMC7MXMA2AR5
- Solicitation number
- 2015.1
- Topic code
- AF151-073
Research abstract
Modular engines utilize a number of small combustion chambers, called thrust cells, arrayed around an aerospike nozzle. This type of engine has many benefits including high performance and small combustion devices that can be inexpensively built and test
Technology keywords
Not reported
Other awards by this recipient
Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.
- High Response Control Valve
- High Response Control Valve
- Predicting the Flow Interactions of Modular Liquid Rocket Engine Thrust Chambers
- Fast Acting Flow Control Valve
- Fast Acting Flow Control Valve
Awards with the same topic code
Verified by an exact topic code match. This is not a text-similarity match.
Research funding history
17 SBIR/STTR records share this UEI (2003–2018). Reported award amounts total $7,350,835. Reported amounts are not federal obligations.
Phases: Phase I, Phase II
Agencies: Department of Defense, National Aeronautics and Space Administration