The Hall-engine-based Electric Jet Propulsion System (EJPS) is designed for spacecraft orbit correction, stabilization, and interplanetary flights.
Basic Specifications
|
Working medium - xenon |
|
|
Maximum bottle pressure at 50°С, MPa |
13 |
|
Total thrust impulse, kN·s |
50 - 1000 |
|
Nominal Hall engine thrust, mN |
1 - 66 |
|
Thrust excursion in all operating environments, % |
15 |
|
Specific impulse of Hall engines in continuous running mode in nominal environment, m/s |
2200 -22000 |
|
Engine thrust-to-power ratio, W/mN |
16-20 |
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