Venera 3MV-1
Venera 8
Credit - NASA
Other Designations: Zond 1. Manufacturer's Designation: 3MV-1. Class: Planetary. Type: Venus. Destination: Venus. Nation: Russia. Agency: NII-88. Manufacturer: Lavochkin.

Typical orbit: 197 km x 209 km at 65 degrees inclination. Mass: 890 kg (1,960 lb). Associated Launch Vehicle: Molniya 8K78M.


Venera 3MV-1 Chronology
  • 1964 April 2 - Zond 1 - Program: Venera. Launch Site: Baikonur. Launch Vehicle: Molniya 8K78M. Mass: 890 kg (1,960 lb).

    Failed Venus probe. Solar Orbit (Heliocentric). Elaboration of a long range space system and conduct of scientific research.

  • 1964 March 1 - Venus launch delayed. - Program: Venera. Launch Site: Baikonur. Launch Vehicle: Molniya 8K78M.

    The launch was delayed due to malfunctions during prelaunch service.

  • 1964 March 27 - Cosmos 27 - Program: Venera. Launch Site: Baikonur. Launch Vehicle: Molniya 8K78M. FAILURE: During unpowered coast in parking orbit the escape stage Block L lost stable attitude due to a loss of the the power circuit of the pneumatic valves of the attitude control and stabilisation system. Mass: 890 kg (1,960 lb). Perigee: 197 km (122 mi). Apogee: 209 km (129 mi). Inclination: 64.80 deg. Period: 88.50 min.

    The stage with payload remained in Earth orbit as Cosmos-27.


Bibliography and Further Reading
  • 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.
  • 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
  • Novosti Kosmonavtiki, "Otmenenniy Start "Molniya-M"", 1997, Issue 1, page 29.
 
 
 
 
 
 
 
 
 

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