Electromagnetic systems protecting spacecraft from the orbital FRAGMENTS

摘要

Electromagnetic system of protection of spacecraft (SC) of the orbital debris refers to the spacecraft system of protection against orbital debris or space "garbage". Electromagnetic system for protecting spacecraft from orbital fragments comprises at least two protective plates of electrically conductive material set in isolation to each other in the direction of flight of orbital debris and connected in parallel to the pulse voltage source (AC), a sensor contact orbital debris mounted on the outside in the direction flight orbital debris protective plate and the amplifier-shaper, the output of orbital debris contacts the sensor via the amplifier-shaper conn nen with the triggering input voltage (current) source made in the form of a controlled pulse voltage of the pulse generator (AC), such as explosive magnetic generator. Thanks to said plurality of characteristic features obtained technical result, namely: improved reliability, economy and safety of operation of the device by applying a momentary voltage (current) pulse on the protective plate only at the time of collision orbital fragment with external direction of its flight the protective plate, as well as simplified construction device because there is no need of partitioning the shield plates and weight of the device is reduced.; 1 bp 7 ZP f ly-4-yl.