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Vega 1, 2 (5VK #1, 2)
 Vega 1 |
 Vega 1 Lander |
Vega (Venera Gallei) was combined mission to Venus, where the fly-by bus released a lander and to comet 1P/Halley.
| Nation: | USSR |
|---|---|
| Type / Application: | Venus flyby, Comet Halley flyby |
| Operator: | |
| Contractors: | |
| Equipment: | |
| Configuration: | |
| Propulsion: | |
| Power: | 2 deployable fixed solar arrays, batteries (probe); batteries (lander) |
| Lifetime: | |
| Mass: | |
| Orbit: |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| Vega 1 (5VK #1) | 1984-125A | 15.12.1984 | Ba LC-200/39 | Proton-K Blok-D-1 | ||
| Vega 2 (5VK #2) | 1984-128A | 21.12.1984 | Ba LC-200/40 | Proton-K Blok-D-1 |
Further Venera missions:
- Vega 1, 2 (5VK #1, 2)
- Venera 1 (1VA #1, 2)
- Venera (2MV-1 #1, 2)
- Venera (2MV-2 #1)
- Venera 2 (3MV-4 #3, 4)
- Venera 3 (3MV-3 #1)
- Venera 4 (V-67 #1, 2)
- Venera 5, 6 (V-69 #1, 2)
- Venera 7 (V-70 #1, 2)
- Venera 8 (V-72 #1, 2)
- Venera 9, 10, 11, 12 (4V1 #1, 2, 3, 4)
- Venera 13, 14 (4V1M #1, 2)
- Venera 15, 16 (4V2 #1, 2)
- Venera D
- Zond 1 (3MV-1 #1, 2)
- Zond (3MV-1A #1, 2)
