DEVICE FOR SUPPLYING POWER TO AN AEROSPACE VEHICLE, ASSOCIATED SYSTEM FOR CONTROLLING ELECTRIC ACTUATORS OF A SPACE LAUNCHER AND SPACE LAUNCHER

摘要

power supply device of an aerospace craft, comprising a power supply potential and a conduit (9) is configured to be connected to the machine body (10) of the aerospace object in two areas of the voltages (3)(4) within each of which the electric potential difference does not exceed the critical voltage of the paschen law, each area (3, 4) comprising an electrical insulation is independent.