Applicable to satellite platforms of 80~200kg, used for satellite orbit raising, long-term phase maintenance, and deorbiting. The single-coil technology system is simple and reliable, suitable for satellites with high total impulse and low-cost requirements, such as SAR imaging and navigation enhancement. The product has high technological maturity, with on-orbit flight experience and high performance indicators.
Technical Features:
1. Multi-mode operation to meet different thrust requirements.
2. The lanthanum hexaboride cathode has stronger oxidation resistance and longer lifespan characteristics, while the barium-tungsten cathode has low power consumption, making it more suitable for low-power output satellite platforms.
3. Outstanding cost advantages, suitable for high total impulse and low-cost requirements.
Serial Number | Parameter | Technical Specification |
1 | Steady-State Thrust (Xenon) | 10~18mN |
2 | Steady-State Specific Impulse (Xenon) | 1100s~1450s |
3 | Steady-State Power (Xenon) | 200W~300W |
4 | Steady-State Thrust (Krypton) | 11~16mN |
5 | Steady-State Specific Impulse (Krypton) | 1316s~1433s |
6 | Steady-State Power (Krypton) | 265W~340W |
7 | Operational Time | Cumulative Single Operation Time ≥ 204 hours; Power Cycle Times ≥ 5500 |
8 | On-Orbit Lifetime | 5~8 Years |
9 | Total Impulse | ≥ 126000 Ns |
10 | Weight (Including Cathode) | 1.0kg ± 0.1kg |
11 | Beam Angle | ≤ 40° |
12 | Peak Power Consumption | ≤ 380W |
13 | Ignition Start Time | 6min ± 1s |
14 | Propellant | Xenon / Krypton |