Gas jet propulsion systems (GJPS) damp spacecraft's initial post-separation disturbances and provide attitude control, orbit correction, and spacecraft spin about any axis.
Basic Specifications
|
Working medium - air, nitrogen, argon |
|
|---|---|
|
Maximum bottle pressure at 20°С, MPa |
23 |
|
Nominal gas pressure upstream engines, MPa |
0,3 |
|
Total thrust impulse, N·s |
250 - 7000 |
|
Nominal engine thrust, N |
0,1; 0,2; 8,5 - 55 |
|
Thrust excursion in all operating environments, % |
±25 |
|
Specific impulse in 20°C air, m/s |
710 |
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