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SPACEBUS NEO

 

Satellite Platform Spacebus NEO
Manufacturer Thales Alenia Space
Dimensions -
Platform Wet Mass up to 7600 kg
Payload Mass up to 2000 kg
Applications TV Broadcast, High Throughput Broadband, Mobility/Cellular backhaul, Government/Military, Meteorology
Lifetime 15 years
Payload Power up to 20 kW
Solar Array Power 20+ kW
Frequency Bands Ku / Ka / S / C / X / L / EHF / SHF / UHF
Attitude Control Accuracy ±0.05 deg.
Propulsion System Full electric
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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