Aerospace Instrument-Making Annotation << Back The device for detection of outflow of air from the International space station Н.Д Сёмкин, В.Л. Балакин, К.Е. Воронов, А.В. Пияков The computational parameters of a linac design for imitation of space dust plasma permitting are submitted the theory to accelerate charged microparticles a dia from 0,05 up to 10 microns in speed range 0,1 - 45 kmЧsec-1. of micrometeorites. The simulator has 27 accelerating intervals, to each of which the accelerating potential, equal 30 sq is applied. The fragments are injected in the linac after preacceleration in a linear electrostatic booster with the effective voltage 300 kV. The general effective accelerating voltage of the tendered booster makes 1,11 МV. The difference of the given linac is, that all handsets of drift have the identical sizes, but their accelerating voltage on them is reshaped for each accelerated fragment individually