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AKA: 1V;1V (V-67). Status: Operational 1967. First Launch: 1967-06-12. Last Launch: 1967-06-17. Number: 2 . Gross mass: 1,105 kg (2,436 lb). The descent vehicle carried two thermometers, a barometer, a radio altimeter, an atmospheric density gauge, 11 gas analyzers, and two radio transmitters operating in the DM waveband. The main bus, which carried the capsule to Venus, had a magnetometer, cosmic ray detectors, hydrogen and oxygen indicators, and charged particle traps. Signals were returned by the spacecraft, which braked and then deployed a parachute system after entering the Venusian atmosphere, until it reached an altitude of 24.96 km.
More at: Venera 1V (V-67). Family: Venus. Country: Russia. Engines: KDU-414. Launch Vehicles: R-7, Molniya 8K78M. Projects: Venera. Launch Sites: Baikonur, Baikonur LC1. Agency: MOM, Lavochkin bureau. Bibliography: 2, 296, 6, 64, 65, 13329.
1967 June 12 - . 02:39 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
1967 June 17 - . 02:36 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Molniya 8K78M. FAILURE: Stage 4's engine 11D33 failed to ignite because the turbopump had not been cooled before ignition.. Failed Stage: U.
1967 October 18 - .
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