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Manufacturer's Designation: 36KS. Class: Earth. Type: Magnetosphere. Destination: Maximum Payload Orbit. Nation: Russia. Agency: MOM. Manufacturer: Kozlov. Science. Adaptation of the Vostok spacecraft. Typical orbit: 214 x 399 km, 62.7 deg inclinaton. Mass: 6,300 kg (13,800 lb).
Efir Chronology - 1984 March 10 - Cosmos 1543 - Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 6,300 kg (13,800 lb). Perigee: 214 km (132 mi). Apogee: 401 km (249 mi). Inclination: 62.80 deg. Period: 90.70 min. Duration: 26.00 days.
Scientific mission using spacecraft based on Vostok/Zenit design.
- 1985 December 27 - Cosmos 1713 - Launch Site: Plesetsk. Launch Complex: -. Launch Vehicle: Soyuz. Mass: 6,300 kg (13,800 lb). Perigee: 215 km (133 mi). Apogee: 397 km (246 mi). Inclination: 62.80 deg. Period: 90.60 min. Duration: 26.00 days.
Bibliography:- McDowell, Jonathan, Jonathan's Space Home Page (launch records), Harvard University, 1997-present. Web Address when accessed: http://www.planet4589.org/jsr.html.
- JPL Mission and Spacecraft Library, Jet Propulsion Laboratory, 1997. Web Address when accessed: http://msl.jpl.nasa.gov/home.html.
- Voevodin, Sergey A, VSA072 - Space Apparatus, "Sergey A. Voevodin's Reports", Web Address when accessed: http://home.attbi.com/~rusaerog/spacecraft.html.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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