U.S.S.R. / Russia |
11A511U Progress |
11A511U Progress M/M1/MM/MS |
11A511U2 Progress M |
Soyuz-FG Progress M1/MS |
||
Overall |
Operational | from | 20.01.1978 | 10.08.1993 | 23.08.1989 | 25.09.2002 |
|
to | 05.05.1990 | 22.02.2017 | 22.05.1993 | 16.11.2918 | |
Orbital flights | 43 | 49+8+29+3 | 18 | 3+1 | ||
Payload weight (Mission) | t | 7.12 | 7.20 | 7.28 | 7.28 | |
Gross liftoff weight | t | 313.30 | 311.70 | 311.90 | 311.75 | |
Gross propellant weight | t | 269.71 | 269.71 | 269.66 | 269.71 | |
Total length | m | 47.80 | 46.58 | 46.58 | 45.88 | |
Max. diameter (span) | m | 10.30 | 10.30 | 10.30 | 10.3 | |
Total liftoff thrust (s.l.) | kN | 4,054.2 | 4,054.2 | 4,091.3 | 4,148.6 | |
Total impulse (vac) | MN*s | 835.0 | 835.0 | 843.7 | 849.6 | |
Fairing |
Total length | m | 12.08 (+SAS) | 10.86 | 10.86 | 10.16 |
Diameter | m | 3.00 (2.70) | 3.00 | 3.00 | 3.00 | |
Total weight | t | 3.20 | 1.70 | 1.70 | 1.70 | |
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 | 25.58 | 25.38 | 25.58 | 25.38 | |
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 | 298.2 | |
Specific impulse(vac) | N*s/kg | 3198 | 3198 | 3198 | 3240 | |
Burn time | s | 247 | 247 | 247 | 250 | |
Total impulse (vac) | MN*s | 73.5 | 73.5 | 73.5 | 74.5 | |
Stage 1 |
Name |
Block A | Block A | Block A | Block A | |
Length | m | 27.77 | 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*) | 99.70 (3.12*) | 99.76 (3.12*) | |
Propellant weight | t | 90.10 | 90.10 | 90.05 | 90.10 | |
Engines (Chambers) | RD-118 (4) | RD-118 (4) | RD-118P (4) | RD-108A (4) | ||
Propellant | Kerosene/LOX | Kerosene/LOX | SynTin/LOX | Kerosene/LOX | ||
Total thrust (s.l.) | kN | 777.8 | 777.8 | 814.9 | 792.4 | |
Specific impulse (s.l.) | N*s/kg | 2481 | 2481 | 2579 | 2527 | |
Burn time | s | 287.4 | 287.4 | 285.0 | 287.4 | |
Total impulse (vac) | MN*s | 279.2 | 279.2 | 287.9 | 283.3 | |
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-117 (4) | RD-117 (4) | RD-117 (4) | RD-107A (4) | ||
Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||
Total thrust (s.l.) | kN | 3,276.4 | 3,276.4 | 3,276.4 | 3,356.2 | |
Specific impulse (s.l.) | N*s/kg | 2520 | 2520 | 2520 | 2582 | |
Burn time | s | 120.5 | 120.5 | 120.5 | 120.5 | |
Total impulse (vac) |
MN*s |
482.3 | 482.3 | 482.3 | 491.8 |
* from there hydrogen peroxide and nitrogen |