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Zond 2, 3 / Venera 2 (3MV-4 #1, 2, 3, 4)

Zond-3 (3MV-4 #1)

Nation: USSR
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
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)