ДП «Конструкторське бюро «Південне» ім. М.К. Янгеля»"

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

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