FIELD: electricity.
SUBSTANCE: invention relates to the method and apparatus for reducing the intensity of electrical discharge that occurs in the fluid transportation system in an aerospace vehicle. Operation of the aerospace vehicle. Fluid transportation system in the aerospace vehicle is made of materials selected so that the fluid transportation system has an electrical configuration.
EFFECT: intensity of the electrical discharge that occurs in the fluid transportation system during control of the aerospace vehicle is reduced to acceptable limits by the configuration of the electrical part of the fluid transportation system.
14 cl, 16 dwg
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Authors
Dates
2019-03-25—Published
2013-06-07—Filed