The MONARC-90LT from Moog is a Spacecraft Thruster with a steady state thrust of 90 N and a specific impulse of 232.1 secs. It has a feed pressure range of 5.5-27.6 bar and a nozzle expansion ratio of 40:1. This hydrazine thruster has a minimum impulse bit of 1.8 N-sec and requires a valve power of 72 W. It has a mass of 1.12 Kg and measures 30 cm (engine length). The thruster is suited for spacecraft and flight vehicle attitude control applications and is ideal for earth observation and communication, missile defense, and space exploration missions.
