In December of 2005, one of two trailing umbilical cables used on the International Space Station (ISS) Mobile Transporter (MT) was inadvertently severed by an internal cutter system designed to free a snagged cable or jammed reel while transporting hazardous payloads. The mechanism s intended means of actuation is electrical; however, troubleshooting revealed a mechanical actuation occurred. The investigation of the failed component revealed several lessons learned in developing hardware requirements, understanding and following the rationale behind the requirements throughout the design life cycle, understanding the impacts of gaps and tolerances in a mechanism, and the importance of identifying critical steps during assembly.
Failure of the Trailing Umbilical System Disconnect Actuator on the International Space Station
39th Aerospace Mechanisms Symposium ; 2008 ; Houston, TX, United States
2008-01-01
Conference paper
No indication
English
NTRS | 1970
|NTRS | 1966
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