Low Power Stationary Plasma Thruster with 70 mm Diameter of the Accelerating Channel
Glavkosmos
Thruster. Propellant - xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and four external magnetic coils. Outside diameter of the accelerating channel is 70 mm. Mean diameter of the accelerating channel is 55 mm. Manufacturing lead time is
Technical specifications
- Discharge power
- 669 W
- Discharge voltage
- 300 V
- Discharge current
- 2.23 A
- Thrust
- 39 mN
- Specific impulse
- 1470 s
- Efficiency
- 43%
- Specific power
- 446 W/kg
- Power-to-thrust ratio
- 17.2 W/mN
- Total impulse
- > 0.49 MN∙s
- Mass
- 1.5 kg
About
Thruster. Propellant – xenon. Consists of the anode and cathode units. Classical scheme of the magnetic system with magnetic screens and four external magnetic coils. Outside diameter of the accelerating channel is 70 mm. Mean diameter of the accelerating channel is 55 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.
