Space Hardware Marketplace — Satellite Platforms, Components & Ground Equipment — Page 299

Propulsion

Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XFC Unit)

Glavkosmos

Thrust 0.04 N · Specific impulse 1,470 s · Total impulse 0.5 N·s · Mass 2.8 kg

Consists of two units: M-70 Stationary Plasma Thruster and Xenon Flow Controller Unit (XFC Unit). Propellant - xenon.…

Propulsion

TU1 Thruster Unit Based on Modified Thermocatalytic Low Thruster

Glavkosmos

Mass 0.59 kg · Power 7.3 W

Propellant - hydrazine. The unit consists of one modified thermocatalytic low thruster. Thermal mode of the unit is…

Propulsion

TU3 Truster Unit Based on Modified Thermocatalytic Low Thrusters

Glavkosmos

Mass 1.3 kg · Power 7.3 W

Propellant - hydrazine. The unit consists of three modified thermocatalytic low thrusters. Thermal mode of the unit is…

Propulsion

Xenon Cold Gas Thruster

Glavkosmos

Specific impulse 40 s

Propellant – xenon, nitrogen. The thruster components are: a thermal accumulating chamber with a heater and a nozzle…

Propulsion

Propulsion System [PS] for Nanosatellite Platform

Glavkosmos

Thrust 0.01 N · Mass 1.3 kg · Power 12 W · Supply voltage 5…12 V

Electrothermal propulsion unit for CubeSat-class spacecraft (1.3 kg, 3–10 mN, 25–30 m/s ΔV for 5 kg spacecraft).

Propulsion

Station Keeping Thruster Unit Based on Modified Thermocatalytic Thrusters

Glavkosmos

Mass 1.7 kg · Power 14.6 W

Propellant - hydrazine. The unit consists of two modified thermocatalytic thrusters: 1 – main, and 1 – redundant.…

Propulsion

Station Keeping Thruster Unit Based on Thermocatalytic Thrusters

Glavkosmos

Mass 1.7 kg · Power 14.6 W

Propellant - hydrazine. The unit consists of two thermocatalytic thrusters: 1 – main, and 1 – redundant. Thermal…

Propulsion

Stationary Plasma Thruster with a Discharge Power of up to 25 kW

Glavkosmos

Thrust 1.07 N · Specific impulse 3,200 s · Total impulse 38 N·s · Mass 25 kg

Thruster with a discharge power of up to 25 kW. Propellant - xenon. Development status – engineering model.…

Propulsion

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

Glavkosmos

Thrust 0.19 N · Specific impulse 1,680 s · Total impulse 14 N·s · Mass 8.8 kg

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

Propulsion

Stationary Plasma Thruster with a Discharge Power of up to 6 kW

Glavkosmos

Thrust 0.25 N · Specific impulse 1,850 s · Total impulse 20 N·s · Mass 8.1 kg

Thruster with a discharge power of up to 6 kW. Propellant - xenon. Development status – laboratory model.…

Propulsion

Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W

Glavkosmos

Thrust 0.08 N · Specific impulse 1,600 s · Total impulse 2.6 N·s · Mass 3.5 kg

Thruster with a nominal discharge power of 1350 W. Propellant - xenon. Consists of the anode and cathode…

Propulsion

Modified Stationary Plasma Thruster with a Nominal Discharge Power of 1350 W

Glavkosmos

Thrust 0.09 N · Specific impulse 1,700 s · Total impulse 4.5 N·s · Mass 4.1 kg

Thruster with a nominal discharge power of 1350 W. Propellant - xenon. Consists of the anode and cathode…

Propulsion

Modified Thermocatalytic Low Thruster

Glavkosmos

Mass 0.2 kg

Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a…

Propulsion

Modified Thermocatalytic Thrusters

Glavkosmos

Mass 0.44 kg

Propellant - hydrazine. The main thruster component parts are: a decomposition chamber with a catalyst element and a…

Propulsion

Multichannel Electric Thruster

Glavkosmos

Thrust 0.3 N · Specific impulse 1,500 s · Mass 12 kg · Power 7,500 W

High-power multichannel electric thruster (up to 600 mN, 5–10 kW, Isp 1500–4000 s, 12 kg) for spacecraft propulsion…

Propulsion

Pressure Stabilization Unit

Glavkosmos

Mass 4.5 kg · Power 5 W

Propellant - hydrazine. The unit consists of 2 pressure stabilizers, 6 small-size solenoid valves that supply propellant to…

Propulsion

Propellant Management Assembly (PMA)

Glavkosmos

Mass 3 kg · Supply voltage 10…29 V

PMA is intended for propellant supply to stationary plasma thrusters. It provides an outlet flow rate of not…

Propulsion

Low Power Stationary Plasma Thruster with 50 mm Diameter of the Accelerating Channel

Glavkosmos

Thrust 0.01 N · Specific impulse 860 s · Total impulse 0.13 N·s · Mass 1.23 kg

Thruster. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with…