SBIR/STTR Research Award
Predicting the Flow Interactions of Modular Liquid Rocket Engine Thrust Chambers
Award amount
$149,964Program and phase
SBIR · Phase IAward year
2015Award details
- Awarding agency
- Department of Defense
- Branch
- Air Force
- Recipient company
- WASK Engineering, Inc.
- Proposal award date
- 2015-08-05
- Contract end date
- 2016-03-09
- UEI
- MMC7MXMA2AR5
- Solicitation number
- 2015.1
- Topic code
- AF151-073
Research abstract
ABSTRACT:WASK Engineering will perform trade studies to select design parameters to develop a conceptual design of a modular engine. The purpose of the conceptual design is to provide the requirements for detailed hardware designs of thrust cells and nozzle that will be completed in this effort. The designs will be used for hardware fabrication in a Phase 2 effort. An evaluation will be made of design and analysis tools that will be verified during hardware testing in a subsequent program phase.BENEFIT:This program will put in place critical technologies required to validate the modular rocket engine concept is a cost effective solution for the space launch needs of the US Government. The development and technological risks associated with this type of engine concept will be retired through these efforts.
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