Simulation of a 2250kg two stage rocket to put around 18kg in a LEO (Low Earth Orbit).
This trajectory was selected to improve performance. ALL components of this rocket have been projected so far.
This rocket will use 4 L10K liquid rocket engine and will burn Liquid Oxigen (LOx) and Ethanol (EtOH), generating a total amount of 40kN of thrustin first stage.
The second stage will be propelled by a modified version of L10K called L10K1V
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