Thrust Module (TM) Based on Thruster with 70 mm Diameter of the Accelerating Channel with Xenon Flow Controller Unit (XF
A Thrust Module (TM) for spacecraft station keeping, featuring a 70 mm diameter thruster and a Xenon Flow Controller Unit (XFC Unit). It uses xenon propellant and has significant flight heritage.
Key figurescomparable across the catalogue
- Mass
- 2.8 kg
- Power
- 669 W
- Thrust
- 0.039 N
- Specific impulse
- 1,470 s
- Total impulse
- 0.5 N·s
- Design life
- 0.513 years
- Lead time
- 12 months
Normalised to common units so this product can be compared with others in its category. The supplier's own wording is below.
As published by the supplier
- Purpose
- Spacecraft (S/C) station keeping
- Year of release
- 2001
- Design life
- 4500 hours 3000 cycles years
- Lead time
- 12 months
- Flight qualification of the product
- Yes
- Brief history of flight qualification
- As part of: S/C of Cosmos series; S/C of Luch series (launched on 16.12.94, 11.10.95); Kupon S/C (launched on 16.12.94); S/C of Yamal series (launched on 06.09.99, 24.12.03); KazSat-1 (launched on 18.06.06); KazSat-2 (launched on 16.07.11); Express-MD1 (launched on 11.02.09): Express-MD2 (launched on 06.08.12); EgiptSat-F (launched 22.02.19))
- Possibility to adapt the product to customer requirements
- Yes
- Discharge power
- 669 W
- Discharge voltage
- 300 V
- Discharge current
- 2.23 A
- Thrust
- 39 mN
- Specific impulse
- 1470 s
- Efficiency
- 43%
- Specific power
- 238 W/kg
- Power-to-thrust ratio
- 17.2 W/mN
- Total impulse
- > 0.5 MN∙s
- Mass
- 2.8 kg
About
The Thrust Module (TM) is designed for spacecraft (S/C) station keeping. It was first released in 2001 and boasts a guaranteed service life of 4500 hours and 3000 cycles. The module consists of two main units: an M-70 Stationary Plasma Thruster and a Xenon Flow Controller Unit (XFC Unit). It utilizes xenon as its propellant. The product has undergone flight qualification and has a rich flight heritage, having been deployed on numerous spacecraft including those from the Cosmos series, Luch series (launched on 16.12.94, 11.10.95), Kupon S/C (launched on 16.12.94), Yamal series (launched on 06.09.99, 24.12.03), KazSat-1 (launched on 18.06.06), KazSat-2 (launched on 16.07.11), Express-MD1 (launched on 11.02.09), Express-MD2 (launched on 06.08.12), and EgiptSat-F (launched 22.02.19). The manufacturer offers the possibility to adapt the product to customer requirements. The estimated production/delivery time is 12 months, not including 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.