Engine Model: D-100-II. Manufacturer Name: D-100. Designer: TsNIIMASH. Propellants: Electric/Xenon. Thrust(vac): 0.0650 N (0.0140 lbf). Isp: 1,600 sec. Chambers: 1. Country: Russia. Status: Development. Hall effect thruster with anode layer, designed for satellite orbital raising. Taken to engineering model stage. Thrust 8 to 65 mN, power requirement 1.3 to 15 kW, specific impulse 1600-4250 seconds, efficiency 65%.