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Venera 3MV-4
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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). Associated Launch Vehicle: Molniya 8K78M. Venera 3MV-4 Chronology - 1965 November 12 - Venera 2 - Program: Venera. Launch Site: Baikonur. Launch Vehicle: Molniya 8K78M. 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.
Bibliography and Further Reading
- Novosti Kosmonavtiki, "Otmenenniy Start "Molniya-M"", 1997, Issue 1, page 29.
- Varfolomyev, Timothy, Spaceflight, "Soviet Rocketry that Conquered Space - Part 5", 1998, Volume 40, page 85. 1: Sp 95/37-260; Sp 96/38-31 (8K71 launches); 2: Sp 96/38-48; 3: Sp 96/38-206; Sp 96/38-317 (designatons); 4: Sp 98/40-28; 5:Sp 98/40-85
- McDowell, Jonathan, Jonathan's Space Home Page, Harvard University, 1997-present. Jonathan McDowell's complete on-line listing of all objects orbited and over 20,000 rocket launches Accessed at: http://www.planet4589.org/jsr.html.
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