Development of small regeneratively cooled rocket propulsion systems
The possibility of mixed propellant regenerative cooling for small low cost liquid bi-propellant rocket engines is investigated. Thermochemical analysis have been performed to characterise propellant performance and numerical simulation software has been developed to estimate the thermal performance of a regeneratively cooled N2O ethanol rocket engine. A 100N thrust 3D printed aluminium rocket engine has been designed and tested.
Martin Stengaard Sørensen
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