Electric Propulsion Testing System
Pricing inquiry (see details)
Product Name | Working Dimension(m) | Vac. Level (Torr) | Thrust Capacity (Input Flow) | Temp. Range(°C) | Shroud | Δt (°C/min) |
|---|---|---|---|---|---|---|
2.0 EPTC | 2.0 x 3.0 | < 1x10⁻⁷ | < 20mN (14sccm) | -70°C~ +125°C | Optional | Avg. 3.0°C / min |
4.0 EPTC | 4.0 x 10.0 | < 1000mN (700sccm) | -70°C~ +125°C | Avg. 3.0°C / min |
Korea Aerospace Research Institute (KARI) Electric Propulsion Testing System
Korea Aerospace Research Institute (KARI) Electric Propulsion Testing System
