Concept information
TERME PRÉFÉRENTIEL
METEOSAT-4
DÉFINITION
- Designation: 19876 / 89020B Launch date: 6 Mar 1989 Country of origin: Europe Mission: Meteorology Launch vehicle: Ariane V29 Prime contractor: Aerospatiale Mass at launch: 681 kg Mass in orbit: 316 kg Diameter: 2.1 m Height: 3.1 m Stabilization: Spin stabilized (100 rpm) DC power: BOL: 387 W EOL: 225 W Design lifetime: 5 years Additional information available at "http://www.tbs-satellite.com/tse/online/sat_meteosat_4.html"
CONCEPT GÉNÉRIQUE
URI
https://gcmd.earthdata.nasa.gov/kms/concept/ceb704ea-58eb-441a-8f86-9d2d7017240c
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