title: ÐÐµÑÐ¾Ð´Ñ ÑÐµÐ³Ð¸ÑÑÑÐ°ÑÐ¸Ð¸ Ð¸ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ ÑÐ¸Ð·Ð¸ÑÐµÑÐºÐ¸Ñ Ð¿ÑÐ¾ÑÐµÑÑÐ¾Ð² Ð² Ð¸Ð¾Ð½Ð½Ð¾-Ð¿Ð»Ð°Ð·Ð¼ÐµÐ½Ð½ÑÑ Ð¸ Ð¾Ð¿ÑÐ¸ÑÐµÑÐºÐ¸Ñ Ð¼Ð¾Ð´ÑÐ»ÑÑ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ¾Ð²
title: Ð½Ð°ÑÑÐ½ÑÐ¹ Ð´Ð¾ÐºÐ»Ð°Ð´
titleType: Subtitle
title: Methods for registration and modeling of physical processes in ion-plasma and optical modules of spacecraft
Creators: name: ÐÑÐ±Ð¾, ÐÐ¼Ð¸ÑÑÐ¸Ð¹
Publisher: name: Ð¡Ð°Ð½ÐºÑ-ÐÐµÑÐµÑÐ±ÑÑÐ³ÑÐºÐ¸Ð¹ Ð¿Ð¾Ð»Ð¸ÑÐµÑÐ½Ð¸ÑÐµÑÐºÐ¸Ð¹ ÑÐ½Ð¸Ð²ÐµÑÑÐ¸ÑÐµÑ ÐÐµÑÑÐ° ÐÐµÐ»Ð¸ÐºÐ¾Ð³Ð¾
Year: 2020
Subjects: ÐÐ¾Ð¼Ð¿ÑÑÑÐµÑÐ½Ð¾Ðµ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ
Ð Ð°ÐºÐµÑÐ½ÑÐµ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»Ð¸ ÑÐ»ÐµÐºÑÑÐ¸ÑÐµÑÐºÐ¸Ðµ
ÐÐ°ÐºÑÑÐ¼
Ð±Ð¾ÑÑÐ¾Ð²Ð¾Ð¹ ÑÐµÐ½ÑÐ¾Ñ
Ð¸Ð¾Ð½Ð¸Ð·Ð°ÑÐ¸Ñ
Ð¸Ð¾Ð½Ð½ÑÐ¹ Ð¿Ð¾ÑÐ¾Ðº
Ð¸Ð¾Ð½Ð½ÑÐ¹ ÑÑÐºÐ¾ÑÐ¸ÑÐµÐ»Ñ
onboard sensor
ionization
ion flow
ion accelerator

description: ÐÐºÑÑÐ°Ð»ÑÐ½ÑÐ¼Ð¸ ÑÐ²Ð»ÑÑÑÑÑ ÑÐ¸Ð·Ð¸ÑÐµÑÐºÐ¸Ðµ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ, Ð½Ð°Ð¿ÑÐ°Ð²Ð»ÐµÐ½Ð½ÑÐµ Ð½Ð° ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐºÑ ÑÐ»ÐµÐºÑÑÐ¾ÑÐ°ÐºÐµÑÐ½ÑÑ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»ÐµÐ¹ Ð² ÐºÐ¾Ð¼Ð¿Ð»ÐµÐºÑÐµ Ñ Ð±Ð¾ÑÑÐ¾Ð²Ð¾Ð¹ Ð°Ð²ÑÐ¾Ð¼Ð°ÑÐ¸Ð·Ð¸ÑÐ¾Ð²Ð°Ð½Ð½Ð¾Ð¹ Ð¸ ÑÐµÐ»ÐµÐºÐ¾Ð¼Ð¼ÑÐ½Ð¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð¾Ð¹ ÑÐ¸ÑÑÐµÐ¼Ð¾Ð¹ ÑÐ¿ÑÐ°Ð²Ð»ÐµÐ½Ð¸Ñ Ð´Ð»Ñ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ¾Ð² Ð½Ð¾Ð²Ð¾Ð³Ð¾ Ð¿Ð¾ÐºÐ¾Ð»ÐµÐ½Ð¸Ñ. ÐÐ°Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð¿ÑÐµÐ´Ð¾ÑÑÐ°Ð²Ð»ÑÐµÑ Ð¼ÐµÑÐ¾Ð´Ð¸ÑÐµÑÐºÐ¾Ðµ Ð¾Ð±ÐµÑÐ¿ÐµÑÐµÐ½Ð¸Ðµ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ð¹ ÑÐ¾ÑÐ¾ÑÐµÐ½ÑÐ¾ÑÐ½ÑÑ , ÑÐ»ÐµÐºÑÑÐ¾Ð½Ð½ÑÑ , Ð¸Ð¾Ð½Ð½ÑÑ Ð¸ Ð¸Ð¾Ð½Ð½Ð¾-Ð¿Ð»Ð°Ð·Ð¼ÐµÐ½Ð½ÑÑ Ð¿ÑÐ¾ÑÐµÑÑÐ¾Ð² Ð´Ð»Ñ ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐºÐ¸ ÑÐ»ÐµÐºÑÑÐ¾ÑÐ°ÐºÐµÑÐ½ÑÑ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»ÐµÐ¹ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ¾Ð² Ð½Ð¾Ð²Ð¾Ð³Ð¾ Ð¿Ð¾ÐºÐ¾Ð»ÐµÐ½Ð¸Ñ. Ð¡Ð¿ÑÐ¾ÐµÐºÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð° Ð³ÑÑÐ¿Ð¿Ð° Ð»Ð°Ð±Ð¾ÑÐ°ÑÐ¾ÑÐ½ÑÑ Ð¾Ð±ÑÐ°Ð·ÑÐ¾Ð² Ð´Ð»Ñ Ð¿ÑÐ¾Ð²ÐµÐ´ÐµÐ½Ð¸Ñ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ð¹ Ð² ÑÐ¾Ð¾ÑÐ²ÐµÑÑÑÐ²Ð¸Ð¸ Ñ ÑÐµÐ»ÑÑ Ð¸ Ð·Ð°Ð´Ð°ÑÐµÐ¹ ÑÐ°Ð±Ð¾ÑÑ, Ð²ÑÐ¿Ð¾Ð»Ð½ÐµÐ½ ÑÑÐ°Ð²Ð½Ð¸ÑÐµÐ»ÑÐ½ÑÐ¹ Ð°Ð½Ð°Ð»Ð¸Ð· Ð¸ Ð²ÑÐ±Ð¾Ñ ÐºÐ¾Ð¼Ð¿ÑÑÑÐµÑÐ½ÑÑ Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼Ð½ÑÑ Ð¿Ð°ÐºÐµÑÐ¾Ð² Ð´Ð»Ñ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ð¹ ÑÐ¾ÑÐ¾ÑÐµÐ½ÑÐ¾ÑÐ½ÑÑ , ÑÐ»ÐµÐºÑÑÐ¾Ð½Ð½ÑÑ , Ð¸Ð¾Ð½Ð½ÑÑ Ð¸ Ð¸Ð¾Ð½Ð½Ð¾-Ð¿Ð»Ð°Ð·Ð¼ÐµÐ½Ð½ÑÑ Ð¿ÑÐ¾ÑÐµÑÑÐ¾Ð². ÐÑÑÑÐµÑÑÐ²Ð»ÐµÐ½Ð¾ ÑÐµÑÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð¸Ðµ, Ð°Ð´Ð°Ð¿ÑÐ°ÑÐ¸Ñ Ð¸ Ð¿ÑÐ¸Ð¼ÐµÐ½ÐµÐ½Ð¸Ðµ Ð¿Ð°ÐºÐµÑÐ¾Ð² ÐºÐ¾Ð¼Ð¿ÑÑÑÐµÑÐ½ÑÑ Ð¿ÑÐ¾Ð³ÑÐ°Ð¼Ð¼ COMSOL Ð¸ CST Studio Ð´Ð»Ñ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ð¹ Ð´Ð°Ð½Ð½ÑÑ Ð¿ÑÐ¾ÑÐµÑÑÐ¾Ð². ÐÐ¾Ð»ÑÑÐµÐ½Ñ ÑÐºÑÐ¿ÐµÑÐ¸Ð¼ÐµÐ½ÑÐ°Ð»ÑÐ½ÑÐµ Ð¸ Ð°Ð½Ð°Ð»Ð¸ÑÐ¸ÑÐµÑÐºÐ¸Ðµ ÑÐµÐ¾ÑÐµÑÐ¸ÑÐµÑÐºÐ¸Ðµ ÑÐµÐ·ÑÐ»ÑÑÐ°ÑÑ Ð´Ð»Ñ Ð²ÑÐ±ÑÐ°Ð½Ð½ÑÑ Ð»Ð°Ð±Ð¾ÑÐ°ÑÐ¾ÑÐ½ÑÑ Ð¾Ð±ÑÐ°Ð·ÑÐ¾Ð², Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ ÐºÐ¾ÑÐ¾ÑÑÑ Ð²ÑÐ¿Ð¾Ð»Ð½ÑÐ»Ð°ÑÑ Ð²ÐµÑÐ¸ÑÐ¸ÐºÐ°ÑÐ¸Ñ Ð¿ÑÐ¾Ð²Ð¾Ð´Ð¸Ð¼ÑÑ ÐºÐ¾Ð¼Ð¿ÑÑÑÐµÑÐ½ÑÑ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ð¹. ÐÐ±Ð¾Ð±ÑÐµÐ½Ð½ÑÐ¹ Ð¼ÐµÑÐ¾Ð´ ÐºÐ¾Ð¼Ð¿ÑÑÑÐµÑÐ½Ð¾Ð³Ð¾ Ð¼Ð¾Ð´ÐµÐ»Ð¸ÑÐ¾Ð²Ð°Ð½Ð¸Ñ Ñ Ð¿Ð¾Ð¼Ð¾ÑÑÑ ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐ°Ð½Ð½ÑÑ Ð°Ð´Ð°Ð¿ÑÐ¸ÑÐ¾Ð²Ð°Ð½Ð½ÑÑ Ð¿Ð°ÐºÐµÑÐ¾Ð² CST Ð¸ COMSOL Ð¼Ð¾Ð¶ÐµÑ Ð±ÑÑÑ Ð¾Ð±Ð¾ÑÐ½Ð¾Ð²Ð°Ð½Ð½Ð¾ Ð¸ ÑÑÑÐµÐºÑÐ¸Ð²Ð½Ð¾ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°Ð½ Ð¿ÑÐ¸ ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐºÐµ Ð¸Ð¾Ð½Ð½ÑÑ Ð´Ð²Ð¸Ð³Ð°ÑÐµÐ»ÐµÐ¹ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ¾Ð² Ð½Ð¾Ð²Ð¾Ð³Ð¾ Ð¿Ð¾ÐºÐ¾Ð»ÐµÐ½Ð¸Ñ, Ð² ÑÐ¾Ð¼ ÑÐ¸ÑÐ»Ðµ Ñ Ð°Ð»ÑÑÐµÑÐ½Ð°ÑÐ¸Ð²Ð½ÑÐ¼ ÑÐ°Ð±Ð¾ÑÐ¸Ð¼ ÑÐµÐ»Ð¾Ð¼.
description: A physical research aimed at the development of electric propulsion in combination with an onboard automated and telecommunication control system for new generation spacecraft is relevant. This work provides methodological support for research of photosensor, electronic, ionic and ion-plasma processes for the development of new generation electric propulsion systems for spacecraft. A group of laboratory samples was designed for research in accordance with the aim and the purpose of the work, a comparative analysis and selection of computer software packages for research of photosensory, electronic, ionic and ion-plasma processes were performed. Testing, adaptation and application of COMSOL and CST Studio software packages for research of these processes have been implemented. Experimental and analytical theoretical results were obtained for the selected laboratory samples, on the basis of which the verification of the conducted computer studies was carried out. The generalized method of computer modeling using the developed adapted CST and COMSOL packages can be reasonably and effectively used in the development of ion thrusters for new generation spacecraft, including those with alternative working mass.