Venera 2V (original) (raw)


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Venera 2V


Part of 2MV


Venera 5
Venera 5
Credit: NASA

Russian Venus probe. Spacecraft was very similar to Venera 4 / 1V (V-67) although the descent module was of a stronger design. Venus lander, Russia. Launched 1969.

AKA: Venera V-69. Status: Operational 1969. First Launch: 1969-01-05. Last Launch: 1969-01-10. Number: 2 . Gross mass: 1,128 kg (2,486 lb).

When the atmosphere of Venus was approached, a capsule weighing 405 kg and containing scientific instruments was jettisoned from the main spacecraft. During descent towards the surface of Venus, a parachute opened to slow the rate of descent. For 53 min on May 16, 1969, while the capsule was suspended from the parachute, data from the Venusian atmosphere were returned. The spacecraft also carried a medallion bearing the coat of arms of the U.S.S.R. and a bas-relief of V.I. Lenin to the night side of Venus.


More at: Venera 2V (V-69).


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, 367, 376, 474, 6, 64, 13330.



1969 January 5 - . 06:28 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.


1969 January 10 - . 05:51 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.


1969 May 16 - .


1969 May 16 - .


1969 May 17 - .


1969 May 17 - .



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