|
U.S.S.R |
N-1 / 1 ... . 2L | N-1 / 3L ... 5L | N-1 / 6L ... 7L | N-1F / 8L ... 9L | ||||||
|
Overall Vehicle |
Operational | from | - | 21.02.1969 | 26.06.1971 | 1974 | ||||
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to | - | 03.07.1969 | 23.11.1972 | - | |||||
| Orbital flights | 0 | 2 | 2 | 0 | ||||||
| Payload weight | t | - | - | LEO | ~20 | LEO | ~20 | LEO >> | ~80 | |
| Gross liftoff weight | t | ~2,675 | ~2,709 | ~2,709 | ~2,778 | |||||
| Gross propellant weight | t | 2,493.6 | 2,493.6 | 2,493.6 | 2,501.9 | |||||
| Total length | m | 105.29 | 105.29 | 105.29 | ||||||
| Max. diameter (span) | m | 22.40 | 22.40 | 22.40 | 22.40 | |||||
| Total liftoff thrust (s.l.) | kN | 41,358 | 41,358 | 41,358 | 45,306 | |||||
|
Total impulse (vac) |
MN*s | 7,876.0 | 7,873.4 | 7,892.6 | 8,216.3 | |||||
|
Fairing |
Total length (+SAS) | m | - | 43.72 | 43.72 | 43.72 | ||||
| Diameter | m | - | 5.92 | 5.92 | 5.92 | |||||
| Total weight | t | - | ~15 | ~15 | ~15 | |||||
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Stage 5 |
Name | Block D | Block D | Block D | Block D | |||||
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Length | m | 6.28 | 6.28 | 6.28 | 6.28 | ||||
| Diameter | m | 3.70 | 3.70 | 3.70 | 3.70 | |||||
| Liftoff weight | t | 16 | 16 | 16 | 16 | |||||
| Propellant weight | t | 14.60 | 14.60 | 14.60 | 14.60 | |||||
| Engines | 1 | NK-9V | RD-58 | RD-58 | RD-58 | |||||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||||||
| Total thrust (vac) | kN | 451.1 | 82.60 | 82.60 | 82.60 | |||||
| Specific impulse (vac) | N*s/kg | 3383 | 3393 | 3393 | 3393 | |||||
| Burn time | s | 109.5 | 600 | 600 | 600 | |||||
| Total impulse (vac) | MN*s | 49.4 | 49.6 | 49.6 | 49.6 | |||||
|
Stage 4 |
Name | Block G | Block G | Block G | Block G | |||||
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Length | m | 9.1 | 9.1 | 9.1 | 9.1 | ||||
| Diameter | m | 3.90 | 3.90 | 3.90 | 3.90 | |||||
| Liftoff weight | t | 59 | 59 | 59 | 59 | |||||
| Propellant weight | t | 56.0 | 56.0 | 56.0 | 56.0 | |||||
| Engines | 1 | NK-9V | NK-21 | NK-31 | NK-31 | |||||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||||||
| Total thrust (vac) | kN | 451.1 | 392.3 | 402.1 | 402.1 | |||||
| Specific impulse (vac) | N*s/kg | 3383 | 3334 | 3462 | 3462 | |||||
| Burn time | s | 420 | 480 | 482 | 482 | |||||
| Total impulse (vac) | MN*s | 189.5 | 186.7 | 193.9 | 193.9 | |||||
| Stage 3 |
Name |
Block W | Block W | Block W | Block W | |||||
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|
Length | m | 11.01 (14.1) | 11.01 (14.1) | 11.01 (14.1) | 11.01 (14.1) | ||||
| Diameter | m | 6.8...5.5 | 6.8...5.5 | 6.8...5.5 | 6.8...5.5 | |||||
| Liftoff weight | t | 185 | 185 | 185 | 185 | |||||
| Propellant weight | t | 175.0 | 175.0 | 175.0 | 175.0 | |||||
| Engines | 4 | NK-9V | NK-19 | NK-39 | NK-39 | |||||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||||||
| Total thrust (vac) | kN | 1,804.4 | 1,804.4 | 1,627.9 | 1,627.9 | |||||
| Specific impulse (vac) | N*s/kg | 3383 | 3383 | 3452 | 3452 | |||||
| Burn time | s | 328 | 328 | 371 | 371 | |||||
| Total impulse (vac) | MN*s | 592.1 | 592.1 | 604.1 | 604.1 | |||||
| Stage 2 |
Name |
Block B | Block B | Block B | Block B | |||||
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|
Length | m | 20.46 | 20.46 | 20.46 | 20.46 | ||||
| Diameter | m | 9.8...6.8 | 9.8...6.8 | 9.8...6.8 | 9.8...6.8 | |||||
| Liftoff weight | t | 540.0 | 540 | 540 | 541 | |||||
| Propellant weight | t | 504.6 | 504.6 | 504.6 | 505.4 | |||||
| Engines | 8 | NK-15V | NK-15V | NK-15V | NK-43 | |||||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||||||
| Total thrust (vac.) 100% | kN | 13,182.0 | 13,182.0 | 13,182.0 | 14,058.8 | |||||
| Specific impulse (vac) | N*s/kg | 3187 | 3187 | 3187 | 3393 | |||||
| Burn time | s | 134 | 134 | 134 | 134 | |||||
| Total impulse (vac) | MN*s | 1,608.2 | 1,608.2 | 1,608.2 | 1,715.2 | |||||
| Stage 1 |
Name |
Block A | Block A | Block A | Block A | |||||
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|
Length | m | 30.09 | 30.09 | 30.09 | 30.09 | ||||
| Diameter | m | 16.9....9.8 | 16.9....9.8 | 16.9....9.8 | 16.9....9.8 | |||||
| Liftoff weight | t | 1,874 | 1,874 | 1,874 | 1,882 | |||||
| Propellant weight | t | 1,743.4 | 1,743.4 | 1,743.4 | 1,750.9 | |||||
| Engines | 30 | NK-15 | NK-15 | NK-15 | NK-33 | |||||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | ||||||
| Total thrust (s.l.) 100% | kN | 41,358.3 | 41,358.3 | 41,358.3 | 45,305.7 | |||||
| Specific impulse (s.l.) | N*s/kg | 2785 | 2785 | 2785 | 2915 | |||||
| Burn time | s | 148 | 148 | 148 | 142 | |||||
| Total impulse (vac) | MN*s | 5,436.8 | 5,436.8 | 5,436.8 | 5,683.5 | |||||