A separation system solution for the interim control module

摘要

The Interim Control Module (ICM) is a propulsion and attitude control platform for the International Space Station (ISS) built by the US Naval Research Laboratory (NRL). ICM is delivered to ISS via the Space Shuttle, where it is separated from its structural support canister and moved into docking position using the Shuttle Remote Manipulator System (SRMS). The Pin Extraction Mechanism (PEM) is one of the mechanisms that help ensure the separation of electrical connectors and prevents re-engagement of the pins and sockets. This paper describes the 1CM separation system, the PEM and operational details.