| 1 | A | B | C | D | E | F | G |
| --- | --- | --- | --- | --- | --- | --- | --- |
| 2 | Angara (rocket family) - Cancelled or proposed |  |  |  |  |  |  |
| 3 | Version | Angara 1.1 (Cancelled) | Angara A3 (Proposed) | Angara A5P (Proposed) | Angara A5V (Proposed) | Angara A7 (Proposed) | Angara A7.2B (Proposed) |
| 4 | Boosters | N/A | 2xURM-1 | 4xURM-1 | 4xURM-1 | 6xURM-1 | 6xURM-1 |
| 5 | First stage | 1xURM-1 | 1xURM-1 | 1xURM-1 | 1xURM-1 | 1xURM-1 | 1xURM-1 |
| 6 | Second stage | Briz-KM | Modified Block I | – | URM-2V | KVTK-A7 | URM-2 |
| 7 | Third stage (not used for LEO) | – | Briz-M/RCAF | - | Blok DM-03/KVTK | - | KVTK2-А7В |
| 8 | Thrust (at sea level) | 1.92 MN | 5.77 MN | 9.61 MN | 10.57 MN | 13.44 MN | - |
| 9 | Launch weight | 149 t | 481 t | 713 t | 815 - 821 t | 1133 t | 1323 t |
| 10 | Height (maximal) | 34.9 m | 45.8 m | ? | ? | ? | 65,7 m |
| 11 | Payload (LEO 200 km) | 2.0 t | 14.6 t | 18.0 t | 35 - 40 t | 35 t | 50 t |
| 12 | Payload (GTO) | – | 2.4/3.6 t | – | 11.9 - 13.3 t | 12.5 t | 19 t |
| 13 | Payload (GEO) | – | 1.0/2.0 t | – | 7.2 - 8 t | 7.6 t | 11.4 t |

Question: How does the weight and power of the Angara A7compare to the Angara A5V?
Answer: The proposed Angara A7 weighs 1133 tonnes and capable of putting 35 tonnes into a 200 km orbit or delivering 12.5 tonnes to GTO with KVTK-A7 as the second stage in place of the URM-2.