|
Khrunichev State Research and Production |
Angara 1.2 | Angara 1.2 (PP) | Angara 1.2 (AM) | Angara 5.1 (LM) | Angara- 5 | |||||||
|
Overall Vehicle |
Operational | from | 09.07.2014 | 29.04.2022 | 23.12.2014 | 28.12.2021 | ||||||
| to | 15.10.2022 | 14.12.2020 | ||||||||||
| Orbital flights | 0 | 1 | 2 | 2 | 1 | |||||||
| Payload weight | t | LEO | 4 (?) | Mission | 1.43 | Mission | 1.5 (?) | GTO | 5.00 | GTO | 5.50 | |
| Gross liftoff weight | t | 183.5 | 161.0 | ~163 | 728.8 | ~729.5 | ||||||
| Gross propellant weight | t | 161.61 | 143.78 | ~147 | 660.54 | 660.73 | ||||||
| Total length | m | 41.77 | 41.77 | ~41.40 | 47.77 | |||||||
| Max. diameter (span) | m | |||||||||||
| Total liftoff thrust (s.l.) | kN | 1,922.1 | 1,922.1 | 1,922.1 | 8,918.5 | 8,918.5 | ||||||
| Total impulse (vac) | MN*s | 577.9 | 516.6 | 528 + | 2,371.8 | 2,377.8 | ||||||
|
Fairing |
Total length | m | 9.20 | 9.20 | 9.20 | ~15.20 | ~15.20 | |||||
| Diameter | m | 2.90 | 2.90 | 2.90 | 4.35 | 4.35 | ||||||
| Total weight | t | ~1.00 | ~1.00 | ~1.00 | ~2.00 | ~2.00 | ||||||
| Stage 3 |
Name |
Breeze-KM | AM | Breeze-M | RB DM-03 "Persei" | |||||||
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Length | m | 3.03 (2.56) | 1.49 | 2.65 | |||||||
| Diameter | m | 2.66 (2.48) | 2.80 - 1.19 | 4.10 | ||||||||
| Liftoff weight | t | 6.475 | 22.19 | ~21 | ||||||||
| Propellant weight | t | 5.055 | ? | 19.92 | 18.86 | |||||||
| Engines (Chambers) | S5.98 | 11D458 (4) | S5.98 | RD-58M | ||||||||
| Propellant | UDMH/N2O4 | UDMH/N2O4 | UDMH/N2O4 | RG-1/LOX | ||||||||
| Total thrust (vac) | kN | 19.62 | 1.57 | 19.62 | 85.01 | |||||||
| Specific impulse (vac) | N*s/kg | 3222 | 2989 | 3222 | 3492 | |||||||
| Burn time | s | 830 | ? | 3270 | 775 | |||||||
| Total impulse (vac) | MN*s | 16.3 | ? | 64.2 | 65.8 | |||||||
| Stage 2 |
Name |
URM-2 | URM-2 | URM-2 | URM-2 | URM-2 | ||||||
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|
Length | m | 6.87 | 6.87 | ~6.5 (?) | 6.87 | 6.87 | |||||
| Diameter | m | 3.60 | 3.60 | 2.90 | 3.60 | 3.60 | ||||||
| Liftoff weight | t | 39.746 | 25.33 | ~28.00 | 38.33 | 39.746 | ||||||
| Propellant weight | t | 35.222 | 22.45 | 25.65 (?) | 33.97 | 35.222 | ||||||
| Engines (Chambers) | RD-0124A (4) | RD-0124A (4) | RD-0124A (4) | RD-0124A (4) | RD-0124A (4) | |||||||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | |||||||
| Total thrust (vac) | kN | 296.0 | 296.0 | 296.0 | 296.0 | 296.0 | ||||||
| Specific impulse (vac) | N*s/kg | 3521 | 3521 | 3521 | 3521 | 3521 | ||||||
| Burn time | s | 419 | 267 | 305 (?) | 404 | 419 | ||||||
| Total impulse (vac) | MN*s | 124.0 | 79.0 | 90.3 | 119.6 | 124.0 | ||||||
| Stage 1 |
Name |
URM-1 | URM-1 | URM-1 | URM-1 | URM-1 | ||||||
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|
Length | m | 25.70 | 25.70 | 25.70 | 25.70 | 25.70 | |||||
| Diameter | m | 2.90 | 2.90 | 2.90 | 2.90 | 2.90 | ||||||
| Liftoff weight | t | 132.25 | 132.25 | 132.25 | 132.25 | 132.25 | ||||||
| Propellant weight | t | 121.33 | 121.33 | 121.33 | 121.33 | 121.33 | ||||||
| Engines | RD-191 | RD-191 | RD-191 | RD-191 | RD-191 | |||||||
| Propellant | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | Kerosene/LOX | |||||||
| Total thrust (s.l.) | kN | 1,922.1 (100%) | 1,922.1 | 1,922.1 | 1,230.1 (64%) | 1,230.1 | ||||||
| Specific impulse (s.l.) | N*s/kg | 3052 | 3052 | 3052 | 3052 | 3052 | ||||||
| Burn time | s | 210 | 210 | 210 | 325 | 325 | ||||||
| Total impulse (vac) | MN*s | 437.6 | 437.6 | 437.6 | 437.6 | 437.6 | ||||||
| Booster |
Name |
4 x URM-1 | 4 x URM-1 | |||||||||
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|
Length | m | ~28.50 | ~28.50 | ||||||||
| Diameter | m | 2.90 | 2.90 | |||||||||
| Liftoff weight | t | 529 | 529 | |||||||||
| Propellant weight | t | 485.32 | 485.32 | |||||||||
| Engines | RD-191 | RD-191 | ||||||||||
| Propellant | Kerosene/LOX | Kerosene/LOX | ||||||||||
| Total thrust (s.l.) | kN | 7,688.4 | 7,688.4 | |||||||||
| Specific impulse (s.l.) | N*s/kg | 3052 | 3052 | |||||||||
| Burn time | s | 210 | 210 | |||||||||
| Total impulse (vac) | MN*s | 1,750.4 | 1,750.4 | |||||||||