XCRIT-7 RF Ion Propulsion System
Applicable for satellites weighing 100-200kg, suitable for orbit raising, long-term phase maintenance, and deorbiting. With a specific impulse above 3500s, it is twice that of similar Hall thrusters. For the same mission, it can save more than half of the propellant.
Description
Technical Features:
1. Wide range of thrust adjustment capability
2. Nearly linear adjustment steps
3. High specific impulse, long lifespan
4. Simple structure
No. | Parameter | Technical Index |
1 | Thrust | 10mN |
2 | Specific Impulse | 2900s |
3 | Thruster Weight | ＜1.3Kg |
4 | Power Consumption | 440w |
5 | Cumulative Continuous Operating Time | ≥ 7000h |
6 | Total Impulse | ≥ 250000Ns |
7 | Propellant | Krypton |
8 | Thrust Adjustment Step | 0.1mN |
9 | Propellant Flow Rate | 3.5sccm (Krypton) |
10 | Plume Divergence Angle | ＜ 15° |
11 | Ion Current | 200mA |
contact us
-
Dubai headquarters
Address：
Units 610 & 611, Level 3, The Offices 3, One Central Dubai World Trade Centre, Dubai
Phone：
(+971) 04 594 3961
-
Hong Kong headquarters
Address：
15/F, Data Technology Hub, 5 Chun Cheong Street, Tseung Kwan O Industrial Estate, New Territories, Hong Kong
Phone：
(+852) 2161 8300
-
E-mail
ir@uspace.com
