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High Temperature Electrical System Development Applicable to Supersonic Transports

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Pierro, John J., author.
Conference Name:
National Aerospace Engineering & Manufacturing Meeting
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1962
Summary:
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
Notes:
Vendor supplied data
Publisher Number:
620341
Access Restriction:
Restricted for use by site license

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