Studying the change in characteristics of optical surfaces of a spacecraft


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The change in the working characteristics of the optical element sample depending on the thickness of the contamination film applied to the sample has been estimated experimentally. As sources of contamination, the coatings of lens hoods were chosen, which are located in close proximity to the contamination- sensitive optical system of a spacecraft. A series of experiments for applying contamination films of different thickness to the sample of the optical element has been carried out. Based on preliminary estimations, the thickness of the contamination during the entire period of the active existence of the spacecraft will not exceed 3500 Å.

作者简介

A. Volkov

OAO Korporatsiya Kometa (Kometa Special Space Systems Corporation)

Email: natalya.d.2011@inbox.ru
俄罗斯联邦, Moscow, 115280

N. Dyugaeva

OAO Korporatsiya Kometa (Kometa Special Space Systems Corporation)

编辑信件的主要联系方式.
Email: natalya.d.2011@inbox.ru
俄罗斯联邦, Moscow, 115280

G. Kuvyrkin

Bauman Moscow State Technical University

Email: natalya.d.2011@inbox.ru
俄罗斯联邦, Moscow, 105005

A. Morozov

Bauman Moscow State Technical University

Email: natalya.d.2011@inbox.ru
俄罗斯联邦, Moscow, 105005

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