The ammonia propulsion system (APS) is designed for correction of SC injection error in orbital period and orbital period keeping during active lifetime.
Ammonia Propulsion System for Sich-2M SC

Basic specifications
|
Total thrust pulse, N·s (kgf·s): |
|
|
in hot mode– in cold mode – |
39240 (4000) 13780 (1405) |
|
One engine thrust in hot and cold modes, N (gf) |
0,049 (5) |
|
Thrust deviation from nominal value, %: |
|
|
in hot mode– in cold mode – |
± 15 ± 22 |
|
Number of APS firings during ALT |
up to 1000 |
|
Number of engines, pcs. |
2 |
|
Duration of one firing, min |
20, no more |
|
Specific impulse, m/s (s): |
|
|
in hot mode– in cold mode – |
2500 (255) 882 (90) |
|
Direct-current power voltage, V |
24 to 34 |
|
Maximum power consumption of APS at nominal power voltage of 28 V, W |
472 |
|
APS mass (dry), kg |
40 |
Ammonia Propulsion System for Microsat SC

Basic specifications
|
Total thrust pulse, N·s (kgf·s): |
|
|
in hot mode– in cold mode – |
7000 (714) 2500(255) |
|
One engine thrust in hot and cold modes, N (gf) |
0,049(5) |
|
Thrust deviation from nominal value, %: |
|
|
in hot mode– in cold mode – |
±15 ±22 |
|
Number of APS firings during ALT |
up to 500 |
|
Number of engines, pcs |
2 |
|
Duration of one firing, min |
15, no more |
|
in hot mode– in cold mode – |
2500 (255) 882 (90) |
|
Direct-current power voltage, V |
24 to 34 |
|
Maximum power consumption of APS at nominal power voltage of 28 V, W |
375 |
|
APS mass (dry), kg |
24 |

back to the catalog






















