First Test of KeroLOX Ablative Rocket Engine
This engine uses Kerosene and Liquid Oxygen as propellants, and it has a carbon fiber overwrap and silica insulator to contain the heat and pressure of 800 lbs of thrust.
This engine uses Kerosene and Liquid Oxygen as propellants, and it has a carbon fiber overwrap and silica insulator to contain the heat and pressure of 800 lbs of thrust.