Nasa Wire Harness
Nasa technical standard nasa std 8739 4a with change 1 national aeronautics and space administration washington dc 20546 approved.
Nasa wire harness. The purpose of this nasa technical standard is to set forth requirements for interconnecting cable and harness assemblies that connect electrical electronic or electromechanical components. Former nasa astronaut explains how hygiene is different in space wired duration. Limited life article stock wire and cable with a shelf life exceeding 10 years from manufacturing date shall be segregated and shall not be used on in harness assemblies and hardware. Suggested by canadian broadcasting corp.
Wiring harness connectors of critical components must be capable of withstanding vibration induced stresses. Cable and harness general requirements cont preferred. Astronaut spacewalk realtimetracker nasa feed 24 7 earth viewing cameras space official 5 675 watching live now pilot dies passenger lands king air duration. Cable and harness splices.
Nasa std 8739 7 standard for electrostatic discharge control excluding electrically initiated explosive devices was. Nasa iss fake 1. A splice is the joining of two or more conductors together in a manner that results in a permanent electrical termination and mechanical bond and may be completed by either crimp or solder process. This standard applies to critical work as defined by npd 8730 5.
Connectors shall be straight right angle or flange mount. The proposed research involves modeling the effects of cable harnesses and wiring on the dynamics of spacecraft structures. Completed cable harness assemblies and hardware incorporating silver coated copper wire. 2016 06 30 superseding nasa std 8739 4 with change 6 workmanship standard for crimping interconnecting cables harnesses and wiring measurement system identification.
Crimping interconnecting cables harnesses and wiring nasa std 8739 4 with change 5 fiber optic terminations cable assemblies and installation nasa std 8739 5 with change 1 note. The use of right angle connectors shall be minimized and restricted to applications where stress free mounting of the cable assembly can be assured.