The 1N Monopropellant Thruster from Orbital Propulsion Centre is a Monopropellant Thruster that has a thrust of 0.320 to 1.1 N. This spacecraft thruster has a mass of 0.290 Kg and a specific impulse of 200-223 sec. The thruster consists of an internal redundant catalyst bed heater and provides thermal insulation to guarantee optimum start-up. It is ideal for attitude, trajectory, and orbit control of small satellites and midsize satellites.
