The 450N Thruster (Hydrazine/NTO) from IHI Aerospace is a Spacecraft Thruster with Thrust 450 N, Specific Impulse 329 Sec, Inlet Pressure 1.69 Mpa, 1.62 Mpa. Tags: Hydrazine Thruster, Bipropellant Thruster. More details for 450N Thruster (Hydrazine/NTO) can be seen below.