High Temperature Electrical System Development Applicable to Supersonic Transports 620341
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.
Citation: Pierro, J., "High Temperature Electrical System Development Applicable to Supersonic Transports," SAE Technical Paper 620341, 1962, https://doi.org/10.4271/620341. Download Citation
Author(s):
John J. Pierro
Pages: 12
Event:
Pre-1964 SAE Technical Papers
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Electrical systems
Capacitors
Insulation
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