1700W Hall Thruster (Krypton / Xenon)

Suitable for satellite platforms with a mass of 800~1500 kg, used for satellite orbit raising, long-term phase maintenance, and deorbiting. The dual-cathode design provides higher reliability through redundancy, while the gas flow distribution and new anode configuration technologies achieve efficient ionization of the krypton propellant and high thruster efficiency. The new magnetic shielding technology better reduces ceramic sputtering and concentrates the beam more effectively. Krypton propellant significantly reduces the overall system cost, and its high specific impulse further lowers the total mass of the system.

Description


Technical Features:

1. Multi-mode operation allows real-time adjustment for different thrust levels.

2. Lanthanum hexaboride (LaB₆) cathodes offer superior oxidation resistance and longer lifespan.

3. Krypton propellant provides high specific impulse at low cost, making it particularly suitable for high total impulse scenarios.


Serial Number

Parameter

Technical Specifications

1

Steady-State Thrust (Xenon)

70mN~92mN

2

Steady-State Specific Impulse (Xenon)

1630s~1720s

3

Steady-State Power (Xenon)

1280W~1700W

4

Steady-State Thrust (Krypton)

62mN~80mN

5

Steady-State Specific Impulse (Krypton)

1700s~1810s

6

Steady-State Power (Krypton)

1330W~1720W

7

Operating Time

Cumulative single operation time ≥ 5500h, Switch-on/switch-off cycles ≥ 10000 times

8

On-Orbit Lifetime

5~8 years

9

Total Impulse

≥ 1440000Ns

10

Weight (Dual-Cathode)

4.7kg±0.1kg

11

Peak Power Consumption

≤ 1850W

12

Ignition Startup Time

6min±1s

13

Reliability

0.99, 0.97 (End of Life)

14

Beam Divergence Angle

≤ 30°

15

Propellant

Xenon / Krypton