It features a dual combustion chamber, dual- design and is fueled by a RP-1/LOX mixture
It features a dual combustion chamber, dual- design and is fueled by a RP-1/LOX mixture
It features a dual combustion chamber, dual- design and is fueled by a RP-1/LOX mixture
Two-component closed-cycle liquid-propellant rocket engine with afterburning of oxidizing generator gas after the turbine, equipped with two combustion chambers and two nozzles.
It features a dual combustion chamber, dual- design and is fueled by a RP-1/LOX mixture