Zond-3 (3MV-4 #1)
Nation: | USSR |
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Type / Application: | Mars flyby (Z. 2), Lunar flyby (Z. 3), Venus flyby (V. 2, K. 96) |
Operator: | |
Contractors: | |
Equipment: | |
Configuration: | |
Propulsion: | KDU-414 (S5.19) |
Power: | 2 fixed solar arrays, batteries |
Lifetime: | |
Mass: | 996 kg (3MV-4A), 1037 kg (3MV-4) |
Orbit: |
Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
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Zond 2 (3MV-4 #1) | 1964-078C | 30.11.1964 | Ba LC-1/5 | Molniya | ||
Zond 3 (3MV-4 #2) | 1965-056A | 18.07.1965 | Ba LC-1/5 | Molniya | ||
Venera 2 (3MV-4 #3) | 1965-091A | 12.11.1965 | Ba LC-31/6 | Molniya (M) | ||
Kosmos 96 (Venera (4a)) (3MV-4 #4) | 1965-094A | 23.11.1965 | Ba LC-31/6 | P | Molniya (M) |