Venera 3 (3MV-3 #1)

Venera 3 (3MV-3 #1)

Nation: USSR
Type / Application: Venus flyby and lander
Operator:
Contractors:
Equipment:
Configuration:
Propulsion: KDU-414 (S5.19)
Power: 2 fixed solar arrays, batteries
Lifetime:
Mass: 1042 kg
Orbit:
Satellite COSPAR Date LS Launch Vehicle Remarks
Venera 3 (3MV-3 #1) 1965-092A 16.11.1965 Ba LC-31/6 Molniya (M)

Launch Sites:

  • Ba =   Baikonur (Tyuratam, NIIP-5, GIK-5), Tyuratam, USSR   USSR

Cite this page: