The present invention discloses a separation unlocking mechanism and separation unlocking method based on a rotating
electromagnet, comprising an upper cylinder, a lower cylinder, a locking device, a rotating device, a pushing device, a driving device, a limit pin, a loading nut and a micro switch, wherein the upper cylinder is sleeved on the lower cylinder, the rotating device is installed on the driving device and can rotate with the driving device, the locking device is passed through the upper cylinder and the lower cylinder and abuts against the rotating device, locking the upper cylinder and the lower cylinder together, when the driving device receives a
satellite separation
signal, the rotating device is driven by the driving device to rotate from the abutting position to the disengaging position, releasing the
abutment between the rotating device and the locking device, the locking device is disengaged from the upper cylinder, the upper cylinder and the lower cylinder are unlocked, and the upper cylinder is ejected under the action of the pushing device, completing the
satellite-
rocket separation. The present invention solves the problems of complex structure, high cost, large envelope size and heavy
mass of the
satellite-
rocket separation mechanism.