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Venera 3V (V-70)

Spacecraft · Russia

Original archive entry. The text, images and links below are kept as they were written.

Venera 8
Venera 8
Venera 3V (V-72). Others in the 3V / 3MV series had a similar appearance.
Credit: NASA

Russian Venus probe. Venus lander intended to study the Venusian atmosphere and other phenomena of the planet. Venus lander, Russia. Launched 1970.

After aerodynamic braking, a parachute was deployed, the capsule antenna was extended, and signals were returned. The capsule was the first man-made object to return data after landing on another planet.

Family
Venus
Country
Russia
Engines
KDU-414
Launch Vehicles
R-7, Molniya 8K78M
Projects
Venera
Bibliography
2, 296, 6, 64, 65, 13335

Chronology

3 events

1970 August 17

05:38 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Venera 7 - . Payload: 3V (V-70) s/n 630. Mass: 1,180 kg (2,600 lb). Nation: Russia. Agency: MOM. Program: Venera. Class: Venus. Type: Venus probe. Spacecraft Bus: 3MV. Spacecraft: Venera 3V (V-70). Decay Date: 1970-12-15 . USAF Sat Cat: 4489 . COSPAR: 1970-060A.

    Venera 7 was launched from an earth parking orbit towards Venus to study the Venusian atmosphere and other phenomena of the planet. Venera 7 entered the atmosphere of Venus on December 15, 1970, and a landing capsule was jettisoned. After aerodynamic braking, a parachute system was deployed. The capsule antenna was extended, and signals were returned for 35 min. Another 23 min of very weak signals were received after the spacecraft landed on Venus. The capsule was the first man-made object to return data after landing on another planet.

1970 August 22

05:06 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M. FAILURE: The escape stage Block L's engine 11D33 was late igniting and cut off early at 25 seconds after firing due to abnormal operation of the sequencer and a DC transformer failure.. Failed Stage: U.
  • Cosmos 359 - . Payload: 3V (V-70) s/n 631. Mass: 1,180 kg (2,600 lb). Nation: Russia. Agency: MOM. Program: Venera. Class: Venus. Type: Venus probe. Spacecraft Bus: 3MV. Spacecraft: Venera 3V (V-70). Decay Date: 1970-11-06 . USAF Sat Cat: 4501 . COSPAR: 1970-065A. Apogee: 908 km (564 mi). Perigee: 195 km (121 mi). Inclination: 51.2000 deg. Period: 95.70 min. Probable Venus probe failure..

1970 December 15