TECHNICAL SPECIFICATIONSA MATURE DESIGN FOR A HIGHLY RELIABLE & POWERFUL SATELLITE

In 2 years only, Thales Alenia Space assembled on of their most powerful satellite, for SSI-Monaco.

Platform: SPACEBUS 400 C2
Orbital Position: 52°E
Active Transponders: 38 Ku band 28 for Turkmenistan – 12 for Monaco
3 Beams 

East

West

MENA*

*Middle East North Africa

Solar Array Power: 12 kW
Satellite Launch Mass: 4707 kg 10,377 lb
Satellite Dry Mass: 1,823 kg 4,019 lb
Lifetime: >18 years
Launcher: SpaceX Falcon 9
Launch: 27th April 2015
Flight Proven Technologie and Design

The MonacoSAT satellite is based on the flight proven heritage of 73 Thales Alenia Space Spacebus and more than 300 cumulated years in orbit. The Ku-band payloads are relying on the world leadership in payload manufacturing of Thales Alenia Space (30 to 40 % of the market share).

Features

Low risk solutions with flight proven technologies and high level of quality

Guarantee lifetime of more than 18 years thanks to the large propellant tanks

Mature and proven Ground Segment services and Satellite Control Facility

Operational excellence based on a unique Quality System