The application discloses a space electromechanical thermal fusion type micro driving mechanism, which comprises an external structure and a drive control integrated shaft
system; the external structure comprises a left outer surface
assembly, a right outer surface
assembly, a load support, a back cover plate, a fine measurement lens
assembly, a locking assembly and a
front cover plate; the left outer surface assembly comprises a left shaft
system support, a left connector panel, a left adapter support and a left support locking nut; the right outer surface assembly comprises a right shaft
system support, a right connector panel, a right adapter support and a right support locking nut; the drive control integrated shaft system comprises a core shaft assembly, a control assembly, a bottom cover plate, a connector assembly and a micro stress detection device; the core shaft assembly comprises, from left to right, a core shaft, a left bearing locking nut, a left bearing seat, a left bearing spacer, a left bearing, a
permanent magnet synchronous motor, a right bearing spacer, a right bearing, a right bearing seat and a right bearing locking nut. The application has a long service life, high precision,
programming and
information processing capabilities.