Power supply bus: do not adjust the bus; Bus voltage: 24V-29V; Shunt capacity: 18A/ three stage shunt; Lithium ion battery balancing capacity: 7 way balancing; Charging mode: Automatic charging after separation of star and arrow; Distribution mechanism: Distributed distribution; Number of controllable circuits: ≤15; Dead weight mass: 3Kg.
It mainly completes spacecraft simulation and measurement and control network simulation, including functional modules such as spacecraft digital simulation and measurement and control network digital simulation.
Features: High Performance & High Reliability; Performance parameters: 1)Whole satellite mass：≤100Kg; 2)On-orbit design life:3 years（X100）/5 years（X100T); 4)Pointing accuracy; 3)Load mass：≥50Kg; 5)Three-axis pointing stability; 6)Applications: high resolution remote sensing, high/hyperspectral remote sensing, broadband communication, military applications.
Whole satellite mass：170~250kg； Payload ratio：30%~60%; Output power:≤500W; Life span:3~5 years; Bias momentum pointing accuracy≤0.5°，stability≤0.005°/s； Zero momentum pointing accuracy≤0.1°，stability≤0.001°/s； Measurement and control: uplink 2kbps; downlink 16kbps Data transmission: ≤700Mbps.
The WF series satellite-rocket adapter covers the satellite load of 1kg~1200kg. It adopts screws and mounting flanges to directly connect with the satellite, and the mechanical interface is simple. It can be unlocked through the memory alloy pin puller to realize low-impact unlocking and separation. Main feature: 1) Non pyrotechnic, low impact; 2) Small size, …