Sensors to detect the meteoroid and technological particles, the impact on spacecraft

摘要

The sensor is designed for use in the registration system of meteoroid and man-made space particles acting on the spacecraft. It comprises two electrically conductive plates 1, 2 with a dielectric gasket 3 therebetween, and an electrically heat shield 4 by the impact detected particles. A feature of the sensor is that it further comprises an elastic bumper-screen 5 disposed in front of screen 4. The achieved technical result consists in removing the sensor exposure to the fine fraction meteoroid and manmade waste in size and in preventing accelerated destruction of the sensor of this fine fraction. 1 independent and dependent claims 5, figure 2 of the drawings.