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Efir
Part of Vostok Family
Efir
Efir
Russian earth magnetosphere satellite. Science. Adaptation of the Vostok spacecraft. Cosmic radiation satellite built by TsSKB, Russia. Launched 1984 - 1985. Used Zenit Bus.

AKA: 36KS. Status: Operational 1984. First Launch: 1984-03-10. Last Launch: 1985-12-27. Number: 2 . Gross mass: 6,300 kg (13,800 lb).


More at: Efir.

Family: Earth, Magnetosphere sat. Country: Russia. Engines: 11D82M. Launch Vehicles: R-7, Soyuz-U. Launch Sites: Plesetsk. Agency: MOM, Kozlov bureau. Bibliography: 102, 2, 6, 12300.
Photo Gallery

Cosmos 1713Cosmos 1713
Credit: Manufacturer Image



1984 March 10 - . 17:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Cosmos 1543 - . Payload: Efir s/n 1. Mass: 6,300 kg (13,800 lb). Nation: Russia. Agency: MOM. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Vostok. Spacecraft: Efir. Duration: 26.00 days. Decay Date: 1984-04-05 . USAF Sat Cat: 14797 . COSPAR: 1984-026A. Apogee: 401 km (249 mi). Perigee: 214 km (132 mi). Inclination: 62.8000 deg. Period: 90.70 min. Scientific mission using spacecraft based on Vostok/Zenit design..

1985 December 27 - . 17:06 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz-U.
  • Cosmos 1713 - . Payload: Efir s/n 2. Mass: 6,300 kg (13,800 lb). Nation: Russia. Agency: MOM. Class: Earth. Type: Magnetosphere satellite. Spacecraft Bus: Vostok. Spacecraft: Efir. Duration: 26.00 days. Decay Date: 1986-01-22 . USAF Sat Cat: 16429 . COSPAR: 1985-120A. Apogee: 397 km (246 mi). Perigee: 215 km (133 mi). Inclination: 62.8000 deg. Period: 90.60 min.


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