Development, Verification, and Validation of a Thermal Model for Determining Current Derating Design Limits of Aerospace Wires and Wire Bundles
- Aerospace Standard
Data Sets - Support Documents
|Unnamed Dataset 1|
|Table 1||Wire sizes, wire bundle sizes and insulation types that were used to validate the NASA thermal wire bundle model|
|Table A1||Lab measured resistance for ten-foot silver plated high strength copper alloy conductor in an oil bath at selected temperatures|
|Table A2||A comparison of measured and calculated resistances|
SAE Committee AE-8A, Electrical Wiring and Fiber Optic Interconnect Systems Installation, is associated with those activities directed by the Aerospace Electronics and Electrical Systems Division of SAE and SAE Committee AE-8, Aerospace Electrical/Electronic Distribution Systems which relate to installation and maintenance of electrical wire systems and associated hardware standards and specifications.