Stationary Plasma Thruster with a Discharge Power of up to 25 kW
Glavkosmos
Thruster with a discharge power of up to 25 kW. Propellant - xenon. Development status – engineering model. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and eight external magnetic coils. Outside diameter of the accelerating channel is 230 mm
Technical specifications
- Discharge power
- ≤ 25000 W
- Discharge voltage
- ≤ 800 V
- Discharge current
- (15-48) A
- Thrust
- ≤ 1070 mN
- Specific impulse
- ≤ 3200 s
- Efficiency
- ≤ 60 %
- Specific power
- ≤ 1000 W/kg
- Power-to-thrust ratio
- ≤ 23 W/mN
- Total impulse
- ≤ 38 MN∙s
- Mass
- 25 kg
About
Thruster with a discharge power of up to 25 kW. Propellant – xenon. Development status – engineering model. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and eight external magnetic coils. Outside diameter of the accelerating channel is 230 mm. Mean diameter of the accelerating channel is 200 mm. Manufacturing lead time is given without taking into account the time needed to procure materials (4 months) and procured parts and components (6 months).
Documentation
No public datasheet yet — request the datasheet / ICD from the supplier.
