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Bi-Propelland Liquid Engine

Project type

Extra Curricular Engineering Project

Date

October 2022 - October 2023

Location

Imperial College London Rocketry Society

• Currently developing a closed loop N2O mass flow control system to allow thrust modulation
• Pioneering the accurate modelling of the compressible multiphase liquid N2O for the rocketry society
• Modelling the flow in the Julia programming language for accurate control valve sizing
• Intended for implementation on the 2023 NIMBUS Rocket (Launching at the European Rocketry Challenge 2023)
• Below are some renders of the full rocket with also more details about the entire system

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