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Olympus
Olympus-1
Olympus-1
Credit: Manufacturer Image
European communications technology satellite. This communications technology demonstration satellite tested direct television broadcast beams and was also equipped with conventional communications transponders. Communication, experimental satellite built by British Aerospace BAe (prime); Alenia Spazio, Marconi Space and Alcatel-Bell (payloads) for ESA, International. Launched 1989. Used L-Sat Bus.

Status: Operational 1989. First Launch: 1989-07-12. Last Launch: 1989-07-12. Number: 1 . Gross mass: 2,595 kg (5,720 lb).

It conducted a data relay experiment with ESA's EURECA satellite.

Olympus-1 was a multi-payload communications satellite for direct television broadcast in the bands of the 1977 Geneva Plan of the International Telecommunications Union (ITU) (including a national beam to Italy) plus communication transponders in the 14/12 GHz, 2nd 30/20 GHz bands. Positioned on geostationary orbit at 341 deg E.


More at: Olympus.

Family: Communications technology sat, Geosynchronous orbit, Technology. Country: Europe. Engines: R-4D. Launch Vehicles: Ariane, Ariane 2/3, Ariane 3. Launch Sites: Kourou, Kourou ELA1. Agency: ESA. Bibliography: 2, 279, 6, 6749, 12914.

1989 July 12 - . 00:14 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA1. LV Family: Ariane. Launch Vehicle: Ariane 3.

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