High Temperature Electrical System Development Applicable to Supersonic Transports

620341

01/01/1962

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
Supersonic air transports will require electrical systems capable of withstanding temperatures estimated at 600 F. The suitability of various materials is discussed with respect to use as conductor and as insulation, and components including resistors, transformers, capacitors, rectifiers, and tubes. The Air Force Hotelec program is reviewed with the significant test results. Areas of required additional development work are listed.
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DOI
https://doi.org/10.4271/620341
Pages
12
Citation
Pierro, J., "High Temperature Electrical System Development Applicable to Supersonic Transports," SAE Technical Paper 620341, 1962, https://doi.org/10.4271/620341.
Additional Details
Publisher
Published
Jan 1, 1962
Product Code
620341
Content Type
Technical Paper
Language
English