|
U.S.S.R. / Russia |
11A511 Soyuz 1-21 |
11A511U Soyuz 22-40 (+ASTP) |
11A511U Soyuz T Soyuz TM |
11A511U2 Soyuz T Soyuz TM |
||
|
Overall |
Operational | from | 28.11.1966 | 03.04.1974 | 16.12.1979 | 08.02.1984 |
|
|
to | 06.07.1976 | 14.05.1981 | 25.04.2002 | 03.09.1995 | |
| Orbital flights | 31 | 26 | 13+12 | 6+22 | ||
| Payload weight (Mission) | t | 6.45...6.64 | 6.51...6.86 | 6.85 | 7.07...7.15 | |
| Gross liftoff weight | t | 312.90 | 313.15 | 313.55 | 314.60 | |
| Gross propellant weight | t | 269.71 | 269.71 | 269.71 | 269.66 | |
| Total length (+SAS) | m | 48.47 | 47.80 | 49.20 | 51.32 | |
| Max. diameter | m | 10.30 | 10.30 | 10.30 | 10.30 | |
| Total liftoff thrust (s.l.) | kN | 4,054.2 | 4,054.2 | 4,054.2 | 4,091.3 | |
| Total impulse (vac) | MN*s | 835.0 | 835.0 | 835.0 | 843.7 | |
|
Fairing |
Total length (+SAS) | m | 12.08 | 12.08...12.98 | 13.48...15.59 | 13.48...15.59 |
| Diameter | m | 3.00 (2.70) | 3.00 (2.70) | 3.00 (2.70) | 3.00 (2.70) | |
| Total weight | t | 3.20 | 3.20...3.50 | 3.70...4.50 | 4.50 | |
| Stage 2 |
Name |
Block I | Block I | Block I | Block I | |
| Length (+adapter) | m | 7.95 | 7.95 | 7.95 | 7.95 | |
| Diameter | m | 2.66-3.00 | 2.66-3.00 | 2.66-3.00 | 2.66-3.00 | |
| Liftoff weight | t | 25.66 | 25.66 | 25.58 | 25.58 | |
| Propellant weight | t | 22.98 | 22.98 | 22.98 | 22.98 | |
| Engines (Chambers) | RD-0110 (4) | RD-0110 (4) | RD-0110 (4) | RD-0110 (4) | ||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||
| Total thrust (vac) | kN | 297.5 | 297.5 | 297.5 | 297.5 | |
| Specific impulse(vac) | N*s/kg | 3198 | 3198 | 3198 | 3198 | |
| Burn time | s | 247 | 247 | 247 | 247 | |
| Total impulse (vac) | MN*s | 73.5 | 73.5 | 73.5 | 73.5 | |
| Stage 1 |
Name |
Block A | Block A | Block A | Block A | |
| Length | m | 28.44 | 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 | 2.05-2.95-2.60 | |
| Liftoff weight | t | 99.76 (3.12*) | 99.76 (3.12*) | 99.76 (3.12*) | 99.70 (3.12*) | |
| Propellant weight | t | 90.10 | 90.10 | 90.10 | 90.05 | |
| Engines (Chambers) | RD-118 (4) | RD-118 (4) | RD-118 (4) | RD-118P (4) | ||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | SynTin/LOX | ||
| Total thrust (s.l.) | kN | 777.8 | 777.8 | 777.8 | 814.9 | |
| Specific impulse (s.l.) | N*s/kg | 2481 | 2481 | 2481 | 2579 | |
| Burn time | s | 287.4 | 287.4 | 287.4 | 285.0 | |
| Total impulse (vac) | MN*s | 279.2 | 279.2 | 279.2 | 287.9 | |
| Booster |
Name |
Block B,V,G,D | Block B,V,G,D | Block B,V,G,D | Block B,V,G,D | |
| Length | m | 19.80 | 19.80 | 19.80 | 19.80 | |
| Diameter | m | max. 2.68 | max. 2.68 | max. 2.68 | max. 2.68 | |
| Liftoff weight | t | 177.65 (5.88*) | 177.65 (5.88*) | 177.65 (5.88*) | 177.65 (5.88*) | |
| Propellant weight | t | 156.63 | 156.63 | 156.63 | 156.63 | |
| Engines (Chambers) | RD-107M (4) | RD-117 (4) | RD-117 (4) | RD-117 (4) | ||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||
| Total thrust (s.l.) | kN | 3,276.4 | 3,276.4 | 3,276.4 | 3,276.4 | |
| Specific impulse (s.l.) | N*s/kg | 2520 | 2520 | 2520 | 2520 | |
| Burn time | s | 120.5 | 120.5 | 120.5 | 120.5 | |
| Total impulse (vac) |
MN*s |
482.3 | 482.3 | 482.3 | 482.3 | |
| * from there hydrogen peroxide and nitrogen |