Apparatus and method for measuring parameters of transient plasmas in high-speed impact

Abstract

The invention relates to an apparatus and method for measuring the parameters of transient plasmas in high-speed impact. The apparatus includes a multilayer grid sensor, a power source and an oscilloscope; according to the multilayer grid sensor, the energy of plasmas in space debris impact can be analyzed by using electrified grids, so that parameters including the density, energy and diffusion speed of the plasmas can be obtained; the obtained results are displayed on the oscilloscope; the multilayer grid sensor includes a shielding body, a particle screening grid, an energy scanning grid, a suppression electron grid and a collection electrode which are distributed sequentially from top to bottom; the shielding body is used for shielding an internal electric field, so that voltage applied to each layer of grid can be prevented from affecting an external plasma environment; the particle screening grid is used for distinguishing positive and negative particles; the energy scanning grid obtains energy information of the particles by applying scanning bias voltage; the suppression electron grid not only can prevent the emission of secondary electrons and photoelectrons on the collection electrode, but also can prevent interference on front-end electronics; and the collection electrode is used for collecting the plasmas.

Description

technical field [0001] The invention relates to the aerospace field, in particular to a device and method for measuring transient plasma parameters in ultra-high-speed impacts. Background technique [0002] The impact of space debris on spacecraft materials at ultra-high speed can locally generate a transient plasma environment, which threatens the safe and reliable operation of spacecraft in orbit. The typical speed range of space debris is 1-15km / s. When space debris hits the surface of spacecraft materials at ultra-high speed, part of the kinetic energy will be converted into gasification energy and ionization energy. The ionization of debris and target materials will form a local dense transient plasma cloud. There are two main mechanisms by which the transient plasma cloud formed by the impact of space debris affects the spacecraft. One is that the dense plasma formed by the impact covers the charged area of ​​the spacecraft, causing electrostatic discharge in this are...

AI Technical Summary

Problems solved by technology

Due to the low energy (1-10eV) of the plasma formed by the ultra-high-speed impact of space debris, the plasma will be seriously lost during the diffusion to the sensor, resulting in low collection efficiency

[0006] 2. Insufficiency of the non-contact method for measuring ultra-high-speed impinging transient plasma paramet

Images