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SPACEBUS 4000

 

Satellite Platform Spacebus 4000
Manufacturer Thales Alenia Space
Dimensions 3100 x 2200 x 5500 mm
Platform Wet Mass 3000 - 6000 kg
Payload Mass up to 1400 kg
Applications TV Broadcast, High Throughput Broadband, Mobility/Cellular backhaul, Government/Military, Meteorology
Lifetime 15 years
Payload Power 3 - 12 kW
Solar Array Power 8 - 16 kW
Frequency Bands Ku / Ka / S / C / X / L / EHF / SHF / UHF
Attitude Control Accuracy ±0.05 deg.
Propulsion System Chemical Bi-propellant
Development Time 24 - 30 months
Compatible Launchers Ariane 5, Falcon 9, Atlas V, Proton, H-2A, Long March 3B
Additional Information Single / Dual launch capability

 

 

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