200W Hall Thruster

Description

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