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Venera 8
Credit - NASA
Manufacturer's Designation: 3MV-4. Class: Planetary. Type: Venus. Destination: Venus. Nation: Russia. Agency: MOM. Manufacturer: Lavochkin.

Carried a TV system and scientific instruments.

Typical orbit: 222 km x 296 km at 52 degrees inclination. Mass: 960 kg (2,110 lb).


Venera 3MV-4 Chronology
  • 1965 November 12 - Venera 2 - Program: Venera. Launch Site: Baikonur. Launch Complex: LC31. Launch Vehicle: Soyuz. Mass: 962 kg (2,120 lb). Perigee: 205 km (127 mi). Apogee: 315 km (195 mi). Inclination: 51.80 deg. Period: 89.71 min.
    Venera 2 was launched towards the planet Venus and carried a TV system and scientific instruments. On February 27, 1966, the spacecraft passed Venus at a distance of 24,000 km and entered a heliocentric orbit. The spacecraft system had ceased to operate before the planet was reached and returned no data.

  • 1965 November 23 - Cosmos 96 - Program: Venera. Launch Site: Baikonur. Launch Complex: LC31. Launch Vehicle: Soyuz. FAILURE: At T+528 sec, during the final thrust phase of the Block I's 8D715K engine, one of the combustion chambers blew up due to a tear in the fuel pipeline. This resulted in an abnormal separation of the upper stages. Mass: 960 kg (2,110 lb). Perigee: 222 km (137 mi). Apogee: 296 km (183 mi). Inclination: 51.90 deg. Period: 89.70 min.
    The escape stage Block L entered parking orbit tumbling and was not able to operate properly.


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