Canopus V specifications

Prime contractor NIIEM Federal State Unitary Enterprise, Istra
Mass at launch 460-470 kg
Dry mass 108 kg
Solar array 2 wings
Stabilization 3-axis
DC power 250 W
Design lifetime 5 years

SSTL supplies three suites of satellite avionics and software plus system design support, power management and batteries, on board computers and data handling capabilities for satellite subsystems and satellite operations.
Downlink at 8.048 & 8.3815 GHz (122.88 Mbps)

© TBS Internet, all rights reserved. All reproduction, copy or mirroring prohibited. Legal notice
francais anglais contact