The effect of the environment and extravehicular activity/remote assembly operations on the cables and connectors for spacecraft with metallic and/or nonmetallic structures was examined. Cable and connector philosophy was outlined for the elctrical systems and electronic compartments which contain high-voltage, high-power electrical and electronic equipment. The influence of plasma and particulates on the system is analyzed and the effect of static buildup on the spacecraft electrical system discussed. Conceptual cable and connector designs are assessed for capability to withstand high current and high voltage without danger of arcs and electromagnetic interference. The extravehicular activites required of the space station and/or supply spacecraft crew members to join and inspect the electrical system, using manual or remote assembly construction are also considered.
Cables and Connectors for Large Space System Technology (LSST)
1980
104 pages
Report
Keine Angabe
Englisch
Electromechanical Devices , Electrotechnology , Unmanned Spacecraft , Electric connectors , Electric power transmission , Large space structures , Power lines , Spacecraft electronic equipment , Electromagnetic shielding , Extravehicular activity , High voltages , Human factors engineering , Orbital assembly , Outgassing , Space tools , Wiring
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