Propulsion Angara

                   
RD-191



RD-0124A



RD-0150



RD-0146



RD-0146D

 

Angara 1.2

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

kN

N*s/kg

kN

N*s/kg

tons

s

t/s

MN*s

1

URM-1

RD-191

100%

1,922.1

3052

2,084.3

3310

 121.33 210 0.6298 437.6
2

URM-2

RD-0124A

     296.0 3521 35.22 419 0.0841 124.0
3

Breeze-KM

S5.98

     19.62 3222 5.055 830 0.0061 16.3

 

Angara 1.2PP

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

kN

N*s/kg

kN

N*s/kg

tons

s

t/s

MN*s

1

URM-1

RD-191

100%

1,922.1

3052

2,084.3

3310

 121.33 210 0.6298 437.6
2

URM-2

RD-0124A

     296.0 3521 22.45 267 0.0841 79.0

 

Angara 1.2 /AM

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

kN

N*s/kg

kN

N*s/kg

tons

s

t/s

MN*s

1

URM-1

RD-191

100%

1,922.1

3052

2,084.3

3310

 121.33 210 0.6298 437.6
2

URM-2

RD-0124A

     296.0 3521 25.65 (?) 305 (?) 0.0841 90.3
3

AM

11D458 (4)

     1.57          

 

Angara 5.1

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

kN

N*s/kg

kN

N*s/kg

tons

s

t/s

MN*s
 

Booster (1)

RD-191

1,922.1

3052

2,084.3

3310

 121.33 210 0.6298 437.6
1

URM-1

RD-191

100%

 1,922.1 3052 2,084.3 3310 121.33 5 0.6298 437.6
64% 1,230.1 3052 1,334.0 3310 320 0.4030
2

URM-2

RD-0124A

     296.0 3521 33.97 404 0.0841 119.6
3

Breeze-M

S5.98

     19.62 3222 19.92 3,270 0.0061 64.2

 

Angara A-5

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

kN

N*s/kg

kN

N*s/kg

tons

s

t/s

MN*s
 

Booster (1)

RD-191

1,922.1

3052

2,084.3

3310

 121.33 210 0.6298 437.6
1

URM-1

RD-191

100%

1,922.1

3052

2,084.3

3310

 121.33 5 0.6298 437.6

64%

 1,230.1 3052 1,334.0 3310 320 0.4030
2

URM-2

RD-0124AP

     296.0 3521 35.22 419 0.0841 124.0
3

RB DM-03

 RD-58MF

    

49.1

3649

 18.86 1,400 0.0135 68.8

 

Angara A-5V

Engines

Thrust s.l.

Isp s.l.

Thrust vac

Isp vac

Propellant

Burn time

Flow rate

Total Imp

kN

N*s/kg

kN

N*s/kg

tons

s

t/s

MN*s
 

Booster (1)

RD-191M

1,922.1

3052

2,084.3

3310

 121.33 210 0.6298 437.7
1

URM-1

RD-191M

100%

1,922.1

3052

2,084.3

3310

 121.33 5 0.6298 437.6

64%

 1,230.1 3052 1,334.0 3310 320  0.4030
2

URM-2V

RD-0150 (2)

     1,078.7 4599 ~82.00 ~350 0.2345 377.1
3

KVTK

RD-0146D

    

73.5

4609

 ~25.95 1,200 0.0216 119.6