Multi-function bulkhead structure for micro-satellite system

The present invention provides a bulkhead structure for a multifunctional system for micro-satellite, to a spacecraft power system design and configuration. Multifunctional bulkhead support structure comprises a carbon fiber, a lithium ion battery, the charge balancing circuit, an electrical connector, a voltage display section module, set bearing force, power, charge balance and other functions. The multi-function bulkhead structure enables the power subsystem, structural subsystem design and integration of the three state detection subsystem, and considering the long life of the multi-function bulkhead and cooling issues. The present invention has a small size, light weight, long life and good compatibility with the overall satellite, etc., but also by the simulated microgravity flotation satellites application shows: the present invention effectively reduces the weight of the flotation body and the analog satellite increasing the payload of the analog satellite flotation loading space.