FIELD: electricity.
SUBSTANCE: fluid transport system in an aerospace vehicle is made of materials selected in such a way that the fluid transport system has an electrical part. The intensity of the electric discharge that occurs in the fluid transport system during the control of the aerospace vehicle is reduced down to allowable limits due to the configuration of the electrical part of the fluid transport system.
EFFECT: reducing the intensity of the electric discharge that occurs in the fluid transport system of an aerospace vehicle.
15 cl, 16 dwg
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Authors
Dates
2018-02-12—Published
2013-06-07—Filed