Status: Development ended 1988. Thrust: 17.80 kN (4,002 lbf). Unfuelled mass: 41 kg (90 lb). Specific impulse: 300 s. Specific impulse sea level: 200 s. Burn time: 326 s. Diameter: 1.43 m (4.69 ft).
Thrust (sl): 11.900 kN (2,675 lbf). Thrust (sl): 1,209 kgf. Engine: 41 kg (90 lb). Area Ratio: 98. Thrust to Weight Ratio: 44.34.