Space Hardware Marketplace — Satellite Platforms, Components & Ground Equipment — Page 120

Propulsion

Modified Low Power Stationary Plasma Thruster with 70 mm Diameter of the Accelerating Channel

Glavkosmos

Thrust 0.04 N · Specific impulse 1,500 s · Total impulse 1 N·s · Mass 2.4 kg

In terms of discharge power it has been forced up to 1250 W. Propellant - xenon. Consists of…

Propulsion

Modified Stationary Plasma Thruster with a Discharge Power of up to 5 kW

Glavkosmos

Thrust 0.18 N · Specific impulse 1,770 s · Total impulse 14 N·s · Mass 8.1 kg

Thruster with a discharge power of up to 5 kW. Propellant - xenon. Consists of the anode and…

Propulsion

Electric Thruster for Spacecraft with Mass up to 500 kg

Glavkosmos

Thrust 0.02 N · Specific impulse 1,450 s · Mass 2 kg · Power 350 W

Electric propulsion. It has high efficiency at low power.

Propulsion

Electrically Powered Cruise Engine

Glavkosmos

Thrust 0.52 N · Specific impulse 2,580 s · Mass 11.8 kg · Power 10,500 W

Sustainer power thruster for spacecraft.

Propulsion

High-powered Electric Thruster for Spacecraft with Mass up to 3000 kg

Glavkosmos

Thrust 0.2 N · Specific impulse 1,700 s · Mass 8 kg · Power 3,500 W

Electric propulsion. Multimode thruster. Cathodes on the basis of W-Ba emitter.

Propulsion

Integrated Thruster Unit 13

Glavkosmos

Mass 31 kg · Power 50 W

Integrated Thruster Unit (ITU) includes a high-precision thruster orientation mechanism (TOM) and two propulsion systems based on the…

Propulsion

Integrated Thruster Unit

Glavkosmos

Mass 31 kg · Power 50 W

ITU-5000M includes a high-precision Thruster Orientation Mechanism (TOM) and a propulsion system based on the Modified Stationary Plasma…

Propulsion

Electric Thruster for Spacecraft with Mass up to 1500 kg

Glavkosmos

Thrust 0.04 N · Specific impulse 1,860 s · Mass 3.1 kg · Power 930 W

Electric propulsion. It has high specific impulse at relatively low power. The record number of burnings is up…

Propulsion

Electric Thruster for Spacecraft with Mass up to 2500-3000 kg

Glavkosmos

Thrust 0.1 N · Specific impulse 2,680 s · Mass 5.25 kg · Power 2,400 W

Electric propulsion. Record specific impulse and propulsion resource for Hall-effect thrusters.

Propulsion

Electric Thruster for Spacecraft with Mass up to 3000 kg 1

Glavkosmos

Thrust 0.08 N · Specific impulse 1,550 s · Mass 5.2 kg · Power 1,350 W

Electric propulsion. Multimode thruster. Cathodes on the basis of W-Ba emitter.

Propulsion

Electric Thruster for Spacecraft with Mass up to 3000 kg

Glavkosmos

Thrust 0.07 N · Specific impulse 2,680 s · Mass 6 kg · Power 1,650 W

Electric propulsion. High specific impulse. Cathodes on the basis of W-Ba emitter.

Propulsion

Cold Ammonia Corrective Propulsion System

Glavkosmos

Thrust 5,000 N · Mass 17 kg · Power 50 W

Glavkosmos product — Cold Ammonia Corrective Propulsion System. Details on request.

Propulsion

Cool Gas Thruster

Glavkosmos

Thrust 0.73 N · Specific impulse 73 s · Mass 0.11 kg · Supply voltage 27 V

Glavkosmos product — Cool Gas Thruster. Details on request.

Propulsion

Correction Unit (CU) based on Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W and XFC Unit

Glavkosmos

Thrust 0.08 N · Specific impulse 1,600 s · Total impulse 2.6 N·s · Mass 6.5 kg

Consists of two units: Stationary Plasma Thruster with a nominal discharge power of 1350 W and Xenon Flow…

Propulsion

Corrective Propulsion System 95

Glavkosmos

Thrust 0 N · Specific impulse 0.14 s · Mass 20 kg · Power 180 W

Corrective propulsion system (CPS) consists of a monoblock, including an AIPD-95 CPS engine, a BPU-150 device, a set…

Propulsion

Corrective Propulsion System

Glavkosmos

Thrust 0 N · Specific impulse 0.14 s · Mass 8 kg · Power 150 W

The corrective propulsion system of the UD-AIPD consists of a monoblock, including the KNE block, the BIR1, BIR2…

Propulsion

Dual-mode Stationary Plasma Thruster with a Nominal Discharge Power of 2500/1350 W

Glavkosmos

Thrust 0.09 N · Specific impulse 1,700 s · Total impulse 4.5 N·s · Mass 5.7 kg

Dual operating mode: 1.35 / 2.5 kW. Propellant - xenon. Consists of the anode and cathode units. Classical…

Propulsion

Adjustment and Braking Engine

Glavkosmos

Thrust 464 N · Specific impulse 291 s · Mass 8 kg · Supply voltage 27 V

Propulsive burn formation for center of mass velocity variation during spacecraft orbit control and braking.