A separation system is designed to detach the satellite from its launch vehicle (e.g., rocket) or to separate different stages of the satellite system during deployment. A typical satellite separation system consists of several key components, including a bottom frame, separation springs, engagement leaves, spring plungers, a motorized release mechanism, a sliding tube, a retaining compression ring, and an upper ring. The satellite is securely attached to the upper ring, which compresses the separation springs during launch. It is integrated with a payload adapter, a mechanical structure that acts as the interface between the satellites, the separation system, and the launch vehicle.

Once the launch vehicle reaches the designated orbit, it transmits a command signal to the separation system to release the satellite or payload. Upon receiving this command, the motorized release mechanism activates, triggering the mechanical arrangement of the separation system. This action allows the separation springs to expand, generating a controlled spring force that safely propels the payload away from the launch vehicle. This precise and reliable process ensures a smooth and effective satellite deployment, minimizing the risk of damage and enabling the satellite to commence its intended mission.