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Engines Soyuz-M, Aurora, Onega, Soyuz-2-3, Soyuz-3 etc.
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ex Aurora
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Stage |
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-107A |
839.1 | 2582 | 1,020.4 | 3140 | 39.16 | 120.5 | 0.3250 | 123.0 |
|
D064-200 (2) |
(56.15) |
(2510) |
(68.65) |
(3069) |
(0.0224) |
||||
| Core + | NK-33 | 1,505.8 | 2913 | 1,678.2 | 3246 | 0.5170 | |||
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D064-200 (2) |
56.15 |
2510 |
68.65 |
3069 |
0.0224 |
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| Block-LM | RD-0154 | 300.5 | 3560 | 28.10 | 333 | 0.0844 | 100.0 | ||
| Corvet | RD-58MFD | 78.42 | 3668 | 10.20 | 477 | 0.0214 | 37.4 |
Aurora (Yamal)
|
Stage |
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-107A* |
839.1 | 2582 | 1,020.4 | 3140 | 39.16 | 120.5 | 0.3250 | 123.0 |
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D064-200 (2) |
(56.15) |
(2510) |
(68.65) |
(3069) |
(0.0224) |
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| Core + | NK-33M | 1,510.2 | 2913 | 1,683.2 | 3246 | 0.5185 | |||
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RD-0110R (4) |
23.87 | 2560 | 27.86 | 2929 |
0.0093 |
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| Block-I + |
RD-0124A |
300.1 | 3521 | 28.10 | 330 |
0.0852 |
98.9 | ||
| Corvet | RD-58MFD | 78.42 | 3668 | 10.20 | 477 | 0.0214 | 37.4 |
* RD-0155 option
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Soyuz-M (Rus)
|
Stage |
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-107A | 839.1 | 2582 | 1,020.4 | 3140 | 39.16 | 120.5 | 0.3250 | 123.0 |
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D064-200 (2) |
(56.15) |
2510 |
(68.65) |
3069 |
0.0224 |
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| Core + | RD-120M | 718.5 | 2959 | 784.5 | 3230 | 0.2428 | |||
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D064-200 (2) |
56.15 |
2510 |
68.65 |
3069 |
0.0224 |
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| Block-I+ | RD-0124 | 294.3 | 3521 | 28.10 | 336 | 0.0836 | 98.9 | ||
| Fregat | S5.92 | 19.61 | 3207 | 5.35 | 878 | 0.0061 | 17.2 |
Geos (Yamal)
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Stage |
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-107A | 839.1 | 2582 | 1,020.4 | 3140 | 39.16 | 120.5 | 0.3250 | 123.0 |
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D064-200 (2) |
(56.15) |
(2510) |
(68.65) |
(3069) |
(0.0224) |
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| Core + | RD-120K | 784.5 | 2985 | 850.5 | 3236 | 0.2628 | |||
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D064-200 (2) |
56.15 |
2510 |
68.65 |
3069 |
0.0224 |
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| Block-I | RD-0124 | 294.3 | 3521 | 23.00 | 275 | 0.0836 | 81.0 | ||
| Taimyr | RD-161 | 19.61 | 3530 | 5.00 | 900 | 0.0056 | 17.7 |
Soyuz-2.1v
|
Stage |
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 |
| Core mod. | NK-33M | 1,510.2 | 2913 | 1,682.2 | 3246 | 118.80 | 225 | 0.5185 | 284.9 |
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RD-0110R (4) |
24.35 | 2560 | 27.86 | 2929 |
0.0095 |
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| Block-I | RD-0124 | 294.3 | 3521 | 23.00 | 275 | 0.0836 | 81.0 | ||
| Volga | RD-0162 | 2.94 | 3011 | 0.880 | 900 | 0.0010 | 2.6 |
Soyuz-2-3
|
Stage |
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-107A | 839.1 | 2582 | 1,020.4 | 3140 | 39.16 | 120.5 | 0.3250 | 123.0 |
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D064-200 (2) |
(56.15) |
(2510) |
(68.65) |
(3069) |
(0.0224) |
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| Core + | NK-33-1 | 1,918.2 | 3018 | 2,184.9 | 3438 | ||||
| Block-I | RD-0124 | 294.3 | 3521 | 23.00 | 275 | 0.0836 | 81.0 | ||
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Fregat-SB |
S5.92 |
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20.01 |
3268 |
10.00 |
1,635 |
0.0061 |
32.7 |
Soyuz-2-3v
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Stage |
Engines |
Thrust s.l. |
Isp s.l. |
Thrust vac |
Isp vac |
Propellant |
Burn time |
Flow rate |
Total Imp |
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- |
- |
kN |
N*s/kg |
kN |
N*s/kg |
tons |
s |
t/s |
MN*s |
| Booster (1) | RD-107A | 839.1 | 2582 | 1,020.4 | 3140 | 39.16 | 120.5 | 0.3250 | 123.0 |
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D064-200 (2) |
(56.15) |
(2510) |
(68.65) |
(3069) |
(0.0224) |
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| Core + | NK-33-1 | 1,918.2 | 3018 | 2,184.9 | 3438 | ||||
| Block-E | RD-0146E (4) | 392.3 | 4540 | 0.0864 | |||||
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Fregat-SB |
S5.92 |
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20.01 |
3268 |
10.00 |
1,635 |
0.0061 |
32.7 |
Soyuz-3
|
Stage |
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-120.10F* | 794.3 | 2981 | 862.3 | 3236 | 39.16 | 0.2664 | ||
|
D064-200 (2) |
56.15 |
2510 |
68.65 |
3069 |
0.0224 |
||||
| Core ++ | NK-33-1** | 1,918.2 | 3018 | 2,184.9 | 3438 | 0.6355 | |||
| Block-E | RD-0146E (4) | 392.3 | 4540 | 0.0864 | |||||
| Yastreb | RD-0126A | 39.24 | 4609 | 19.70 | 2315 | 0.0085 | 90.8 |
* RD-0155 option
** RD-191M option
Onega
|
Stage |
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-120.10F* | 794.3 | 2981 | 862.3 | 3236 | 39.16 | 0.2664 | ||
|
D064-200 (2) |
56.15 |
2510 |
68.65 |
3069 |
0.0224 | ||||
| Core ++ | RD-191 | 1,922.5 | 3047 | 2,085.4 | 3305 | 0.6310 | |||
| Block-E+ | RD-0146E (4) | 392.3 | 4540 | 0.0864 | |||||
| Yastreb | RD-0126A | 39.24 | 4609 | 19.70 | 2315 | 0.0085 | 90.8 |
* RD-0155 option
