Fluid transport system for preventing electrical discharge

摘要

A method and apparatus for reducing an intensity of an electrical discharge that occurs within a fluid transport system (100) in an aerospace vehicle (106). The aerospace vehicle (106) is operated. The fluid transport system (100) in the aerospace vehicle (106) is comprised of materials selected such that the fluid transport system (100) has an electrical configuration. The intensity of the electrical discharge that occurs within the fluid transport system (100) during operation of the aerospace vehicle (106) is reduced to within selected tolerances by the electrical configuration of the fluid transport system (100). C%4 0)0 o / r.0 ~C.0 CNo L() 0'