Design and development of a regenerative cooling for small liquid engines

The research work carried out has been focused on the design and development of a regenerative cooling system applied to small liquid rocket engines. According to the green philosophy the pair of propellants used are diesel and HTP. Particular attention has been paid to the design to allow a 3D printing realization. The first part of the work summarizes the mathematical predictive code developed, following the design choices, the test matrix configurations and finally the conclusions.