|
TsSKB Progress/ Roskosmos (RK) |
Soyuz-FG Soyuz TMA |
Soyuz-FG Soyuz TMA-M |
Soyuz-FG Soyuz MS |
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|
Overall |
Operational | from | 30.10.2002 | 08.10.2010 | 07.07.2016 |
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to | 14.11.2011 | 18.03.2016 | 25.09.2019 | |
| Orbital flights | 22 | 20 | 14 | ||
| Payload weight (Mission) | t | 7.30 | 7.30 | 7.30 | |
| Gross liftoff weight | t | 314.60 | 314.60 | 314.60 | |
| Gross propellant weight | t | 269.71 | 269.71 | 269.71 | |
| Total length | m | 51.32 | 51.32 | 51.32 | |
| Max. diameter | m | 10.30 | 10.30 | 10.30 | |
| Total liftoff thrust (s.l.) | kN | 4,148.6 | 4,148.6 | 4,148.6 | |
| Total impulse (vac) | MN*s | 849.6 | 849.6 | 849.6 | |
|
Fairing |
Total length | m | 15.59 (+SAS) | 15.59 (+SAS) | 15.59 (+SAS) |
| Diameter | m | 3.00 | 3.00 | 3.00 | |
| Total weight | t | 4.50 | 4.50 | 4.50 | |
| Stage 2 |
Name |
Block I | Block I | Block I | |
| Length (+adapter) | m | 7.95 | 7.95 | 7.95 | |
| Diameter | m | 2.66-3.00 | 2.66-3.00 | 2.66-3.00 | |
| Liftoff weight | t | 25.38 | 25.38 | 25.38 | |
| Propellant weight | t | 22.98 | 22.98 | 22.98 | |
| Engines (Chambers) | RD-0110 (4) | RD-0110 (4) | RD-0110 (4) | ||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||
| Total thrust (vac) | kN | 298.2 | 298.2 | 298.2 | |
| Specific impulse(vac) | N*s/kg | 3240 | 3240 | 3240 | |
| Burn time | s | 250 | 250 | 250 | |
| Total impulse (vac) | MN*s | 74.5 | 74.5 | 74.5 | |
| Stage 1 |
Name |
Block A | Block A | Block A | |
| Length | m | 27.77 | 27.77 | 27.77 | |
| Diameter | m | 2.05-2.95-2.60 | 2.05-2.95-2.60 | 2.05-2.95-2.60 | |
| Liftoff weight | t | 99.76 (3.12*) | 99.76 (3.12*) | 99.76 (3.12*) | |
| Propellant weight | t | 90.10 | 90.10 | 90.10 | |
| Engines (Chambers) | RD-108A (4) | RD-108A (4) | RD-108A (4) | ||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||
| Total thrust (s.l.) | kN | 792.4 | 792.4 | 792.4 | |
| Specific impulse (s.l.) | N*s/kg | 2527 | 2527 | 2527 | |
| Burn time | s | 287.4 | 287.4 | 287.4 | |
| Total impulse (vac) | MN*s | 283.3 | 283.3 | 283.3 | |
| Booster |
Name |
Block B,V,G,D | Block B,V,G,D | Block B,V,G,D | |
| Length | m | 19.80 | 19.80 | 19.80 | |
| Diameter | m | max. 2.68 | max. 2.68 | max. 2.68 | |
| Liftoff weight | t | 177.65 (5.88*) | 177.65 (5.88*) | 177.65 (5.88*) | |
| Propellant weight | t | 156.63 | 156.63 | 156.63 | |
| Engines (Chambers) | RD-107A (4) | RD-107A (4) | RD-107A (4) | ||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||
| Total thrust (s.l.) | kN | 3,356.2 | 3,356.2 | 3,356.2 | |
| Specific impulse (s.l.) | N*s/kg | 2582 | 2582 | 2582 | |
| Burn time | s | 120.5 | 120.5 | 120.5 | |
| Total impulse (vac) |
MN*s |
491.8 | 491.8 | 491.8 | |
|
*from there hydrogen peroxide and nitrogen |