Projects
Arrax
Rocket engine - LOX/ETH - 1 kN (225 lbf) - 10 bar (145 psi) of chamber pressure - test bench
Igniter
Augmented spark igniter - GOX/ETH - test bench
viserion
Rocket engine - LOX/CH4 - 10kN (2250 lbf) - 40 (580 psi) bars of chamber pressure
