A multi-parameter sensing and bearing integrated structural plate for space is characterized by comprising a
front panel, an inner plate, an outer frame, a distributed
optical fiber sensor, a
vibration sensor, a multi-core photoelectric connector and a
pressure sensor. The inner plate is embedded in the outer frame, and the four corners of the inner plate are each provided with a
pressure sensor. A plurality of
honeycomb grooves are formed in the upper end surface of the inner plate; vibration sensors are fixed in part of the
honeycomb grooves; a multi-core photoelectric connector is fixed at one angular position of the inner plate; each
vibration sensor is connected with the multi-core photoelectric connector; the
front panel covers the inner plate, and a distributed
optical fiber sensor is fixed on the lower end face of the
front panel. According to the structural plate, various sensors are mounted in the structural plate in a nesting and stacking manner, so that the structural plate can measure various parameters; and meanwhile, the structural plate directly transmits the pressure to the mounting main body through the outer frame, so that a
stroke gap is eliminated, and the
pressure sensor does not need to generate
relative displacement and directly measures the external absolute pressure amount.