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astronautix.com NATO 3


Class: Communications. Type: Military. Nation: NATO.

Military communications.


Specification

Total Mass: 720 kg.


NATO 3 Chronology


22 April 1976 NATO 3A Program: NATO. Launch Site: Cape Canaveral . Launch Vehicle: Delta 2914. Mass: 310 kg. Perigee: 35,799 km. Apogee: 36,013 km. Inclination: 10.7 deg.

Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).


28 January 1977 NATO 3B Program: NATO. Launch Site: Cape Canaveral . Launch Vehicle: Delta 2914. Mass: 701 kg. Perigee: 37,079 km. Apogee: 37,421 km. Inclination: 10.5 deg.

Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C).


19 November 1978 NATO 3C Program: NATO. Launch Site: Cape Canaveral . Launch Vehicle: Delta 2914. Mass: 720 kg. Perigee: 36,279 km. Apogee: 36,310 km. Inclination: 7.6 deg.
14 November 1984 NATO 3D Program: NATO. Launch Site: Cape Canaveral . Launch Vehicle: Delta 3914. Mass: 320 kg. Perigee: 35,779 km. Apogee: 35,796 km. Inclination: 2.2 deg.

Stationed at 138 deg W.



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Last update 12 March 2001.
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© Mark Wade, 2001 .