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SolidworksDassault Systems
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Singapore Polytechnic Liquid Rocket Engine Thrust Chamber
This project is a Final Year Project at Singapore Polytechnic under the School of Mechanical and Aeronautical Engineering. Earlier on in the year, we have embarked on the "Heatsink" engine test campaign to get data on the heat flux of the combustion chamber so that the data can be used to inform this current design. The overarching goal of the project is to develop core capabilities such as Regen Cooling, Throttling and Thrust Vector Control which would then be used for a future Vertical Take-off Vertical Landing Hopper Vehicle.
Other than that, this engine uses a pintle injector with a film cooling slot, i will upload the hardware files as the documentation needs to be done first.
You can view data and highspeed camera collected from the project here:
https://drive.google.com/drive/folders/1Ws7XUORCNVCNuSjDNCrcwtus4d81rYfT?usp=sharing
Singapore Polytechnic Liquid Rocket Engine Thrust Chamber
*PCBWay community is a sharing platform. We are not responsible for any design issues and parameter issues (board thickness, surface finish, etc.) you choose.
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