title: Ð ÐµÐ°Ð»Ð¸Ð·Ð°ÑÐ¸Ñ ÑÐ¸ÑÑÐµÐ¼Ñ Ð¾Ð±ÐµÑÐ¿ÐµÑÐµÐ½Ð¸Ñ ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð³Ð¾ ÑÐµÐ¶Ð¸Ð¼Ð° Ð¾ÑÐ½Ð¾Ð²Ð½ÑÑ Ð±Ð»Ð¾ÐºÐ¾Ð² ÑÐ»ÐµÐºÑÑÐ¾Ð½Ð¸ÐºÐ¸ Ð² Ð¼Ð°Ð»ÑÑ ÐºÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ñ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÐ°Ñ Ð½Ð°Ð½Ð¾ÐºÐ»Ð°ÑÑÐ°
title: Ð²ÑÐ¿ÑÑÐºÐ½Ð°Ñ ÐºÐ²Ð°Ð»Ð¸ÑÐ¸ÐºÐ°ÑÐ¸Ð¾Ð½Ð½Ð°Ñ ÑÐ°Ð±Ð¾ÑÐ° Ð¼Ð°Ð³Ð¸ÑÑÑÐ°
titleType: Subtitle
title: Realization of a thermal management system for the main electronic components of small nanoclass spacecraft
Creators: name: Ð¡ÑÐµÐ¿Ð°Ð½Ð¾Ð², ÐÐ¸ÐºÐ¸ÑÐ°
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: 2024
Subjects: ÐÐ¾ÑÐ¼Ð¸ÑÐµÑÐºÐ¸Ðµ Ð»ÐµÑÐ°ÑÐµÐ»ÑÐ½ÑÐµ Ð°Ð¿Ð¿Ð°ÑÐ°ÑÑ
ÐÐºÐºÑÐ¼ÑÐ»ÑÑÐ¾ÑÐ½ÑÐµ Ð±Ð°ÑÐ°ÑÐµÐ¸
ÑÐ¸ÑÑÐµÐ¼Ð° Ð¾Ð±ÐµÑÐ¿ÐµÑÐµÐ½Ð¸Ñ ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð³Ð¾ ÑÐµÐ¶Ð¸Ð¼Ð°
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ÑÐºÑÐ°Ð½Ð½Ð¾-Ð²Ð°ÐºÑÑÐ¼Ð½Ð°Ñ ÑÐµÐ¿Ð»Ð¾Ð¸Ð·Ð¾Ð»ÑÑÐ¸Ñ
thermal management system
nanosatellite
screen-vacuum thermal insulation

description: ÐÐ±ÑÐµÐºÑ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ â ÑÐ¸ÑÑÐµÐ¼Ð° Ð¾Ð±ÐµÑÐ¿ÐµÑÐµÐ½Ð¸Ñ ÑÐµÐ¿Ð»Ð¾Ð²Ð¾Ð³Ð¾ ÑÐµÐ¶Ð¸Ð¼Ð°. Ð¦ÐµÐ»Ñ ÑÐ°Ð±Ð¾ÑÑ â Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ðµ Ð¸ ÑÑÐ¾Ð²ÐµÑÑÐµÐ½ÑÑÐ²Ð¾Ð²Ð°Ð½Ð¸Ðµ Ð¡ÐÐ¢Ð  Ð´Ð»Ñ Ð½Ð°Ð¸Ð±Ð¾Ð»ÐµÐµ ÑÑÐ·Ð²Ð¸Ð¼Ð¾Ð³Ð¾ Ð±Ð»Ð¾ÐºÐ° ÑÐ»ÐµÐºÑÑÐ¾Ð½Ð¸ÐºÐ¸ Ð² ÑÐ¾ÑÑÐ°Ð²Ðµ ÐÐÐ ÑÐ¾ÑÐ¼Ð°ÑÐ° CubeSat Ð½Ð°Ð½Ð¾ÐºÐ»Ð°ÑÑÐ°. Ð ÑÐ¾Ð´Ðµ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ Ð±ÑÐ»Ð¸ Ð²ÑÐ¿Ð¾Ð»Ð½ÐµÐ½Ñ ÑÐ»ÐµÐ´ÑÑÑÐ¸Ðµ Ð·Ð°Ð´Ð°ÑÐ¸: â ÑÐ°ÑÑÐ¼Ð¾ÑÑÐµÑÑ Ð¸Ð· ÐºÐ°ÐºÐ¸Ñ Ð¾ÑÐ½Ð¾Ð²Ð½ÑÑ Ð±Ð»Ð¾ÐºÐ¾Ð² Ð°Ð¿Ð¿Ð°ÑÐ°ÑÑÑÑ Ð¸ Ð±Ð¾ÑÑÐ¾Ð²ÑÑ ÑÐ¸ÑÑÐµÐ¼ ÑÐ¾ÑÑÐ¾Ð¸Ñ ÐÐÐ Ð½Ð°Ð½Ð¾ÐºÐ»Ð°ÑÑÐ°; â ÑÐ°ÑÑÐ¼Ð¾ÑÑÐµÑÑ Ð¿ÑÐ¾Ð±Ð»ÐµÐ¼Ð°ÑÐ¸ÐºÑ ÑÐ°Ð·ÑÐ°Ð±Ð¾ÑÐºÐ¸ Ð¸ Ð²Ð¾Ð·Ð¼Ð¾Ð¶Ð½ÑÐµ Ð¿ÑÐ¾Ð±Ð»ÐµÐ¼Ñ ÑÐ½ÐµÑÐ³Ð¾ÑÐ½Ð°Ð±Ð¶ÐµÐ½Ð¸Ñ Ð¾ÑÐ½Ð¾Ð²Ð½ÑÑ Ð±Ð»Ð¾ÐºÐ¾Ð² Ð°Ð¿Ð¿Ð°ÑÐ°ÑÑÑÑ ÐÐÐ Ð½Ð°Ð½Ð¾ÐºÐ»Ð°ÑÑÐ°; â Ð¸Ð·ÑÑÐ¸ÑÑ Ð¾ÑÐ¾Ð±ÐµÐ½Ð½Ð¾ÑÑÐ¸ Ð¿ÑÐ¸Ð¼ÐµÐ½ÐµÐ½Ð¸Ñ ÐÐÐ Ð½Ð°Ð½Ð¾ÐºÐ»Ð°ÑÑÐ°, Ð° ÑÐ°ÐºÐ¶Ðµ ÑÐ°ÑÑÐ¼Ð¾ÑÑÐµÑÑ ÐºÐ¾Ð½ÑÑÑÑÐºÑÐ¸Ð²Ð½Ð¾âÐºÐ¾Ð¼Ð¿Ð¾Ð½Ð¾Ð²Ð¾ÑÐ½ÑÑ ÑÑÐµÐ¼Ñ Ð´ÐµÐ¹ÑÑÐ²ÑÑÑÐµÐ³Ð¾ ÐÐÐ Ð½Ð°Ð½Ð¾ÐºÐ»Ð°ÑÑÐ° Polytech Universeâ3 (Ð´Ð°Ð»ÐµÐµ â PUâ3); â ÑÐ°ÑÑÐ¼Ð¾ÑÑÐµÑÑ ÑÐ°Ð·Ð»Ð¸ÑÐ½ÑÐµ Ð²Ð¸Ð´Ñ Ð¸ Ð°ÐºÑÑÐ°Ð»ÑÐ½ÑÐµ ÑÐµÐ°Ð»Ð¸Ð·Ð°ÑÐ¸Ð¸ Ð¡ÐÐ¢Ð  ÑÐ»ÐµÐºÑÑÐ¾Ð½Ð¸ÐºÐ¸ Ð¾ÑÐµÑÐµÑÑÐ²ÐµÐ½Ð½ÑÑ Ð¸ Ð·Ð°ÑÑÐ±ÐµÐ¶Ð½ÑÑ ÐÐÐ Ð½Ð°Ð½Ð¾ÐºÐ»Ð°ÑÑÐ°; â ÑÐ°ÑÑÐ¼Ð¾ÑÑÐµÑÑ Ð¡ÐÐ¢Ð  Ð² Ð´ÐµÐ¹ÑÑÐ²ÑÑÑÐµÐ¼ ÐÐÐ PUâ3; â Ð¿ÑÐ¾Ð²ÐµÑÑÐ¸ ÑÐºÑÐ¿ÐµÑÐ¸Ð¼ÐµÐ½ÑÐ°Ð»ÑÐ½Ð¾Ðµ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ðµ ÑÑÑÐµÐºÑÐ¸Ð²Ð½Ð¾ÑÑÐ¸ Ð¡ÐÐ¢Ð  Ð½Ð°Ð¸Ð±Ð¾Ð»ÐµÐµ ÑÑÐ·Ð²Ð¸Ð¼Ð¾Ð³Ð¾ Ð±Ð»Ð¾ÐºÐ° Ð°Ð¿Ð¿Ð°ÑÐ°ÑÑÑÑ ÐÐÐ PUâ3 Ð¸ Ð½Ð° Ð¾ÑÐ½Ð¾Ð²Ðµ Ð¿Ð¾Ð»ÑÑÐµÐ½Ð½ÑÑ Ð´Ð°Ð½Ð½ÑÑ Ð´Ð°ÑÑ ÑÐµÐºÐ¾Ð¼ÐµÐ½Ð´Ð°ÑÐ¸Ð¸ Ð¿Ð¾ ÑÐµÐ°Ð»Ð¸Ð·Ð°ÑÐ¸Ð¸ ÑÑÑÐµÐºÑÐ¸Ð²Ð½Ð¾Ð¹ Ð¡ÐÐ¢Ð . Ð ÐµÐ·ÑÐ»ÑÑÐ°ÑÐ¾Ð¼ Ð¸ÑÑÐ»ÐµÐ´Ð¾Ð²Ð°Ð½Ð¸Ñ ÑÐ²Ð»ÑÑÑÑÑ Ð¿ÑÐµÐ´Ð»Ð¾Ð¶ÐµÐ½Ð¸Ñ Ð¿Ð¾ ÑÑÐ¾Ð²ÐµÑÑÐµÐ½ÑÑÐ²Ð¾Ð²Ð°Ð½Ð¸Ñ Ð¡ÐÐ¢Ð  Ð´ÐµÐ¹ÑÑÐ²ÑÑÑÐµÐ³Ð¾ ÐÐÐ PU-3. ÐÑÐµÐ´Ð»Ð°Ð³Ð°ÐµÑÑÑ Ð¸ÑÐ¿Ð¾Ð»ÑÐ·Ð¾Ð²Ð°ÑÑ ÑÐºÑÐ°Ð½Ð½Ð¾-Ð²Ð°ÐºÑÑÐ¼Ð½ÑÑ ÑÐµÐ¿Ð»Ð¾Ð¸Ð·Ð¾Ð»ÑÑÐ¸Ñ, Ð° ÑÐ°ÐºÐ¶Ðµ ÑÐµÐ°Ð»Ð¸Ð·Ð¾Ð²Ð°ÑÑ ÑÐ¸ÑÑÐµÐ¼Ñ Ð¿Ð¾Ð´Ð°ÑÐ¸ Ð¼Ð¾ÑÐ½Ð¾ÑÑÐ¸ ÑÐ°Ðº, ÑÑÐ¾Ð±Ñ Ð´Ð¾Ð±Ð¸ÑÑÑÑ ÑÐµÑÐ¼Ð¾ÑÑÐ°Ð±Ð¸Ð»Ð¸Ð·Ð°ÑÐ¸Ð¸ Ð±Ð»Ð¾ÐºÐ° ÐÐÐ, Ð° ÑÑÐºÐ¾Ð½Ð¾Ð¼Ð»ÐµÐ½Ð½ÑÑ ÑÐ½ÐµÑÐ³Ð¸Ñ Ð½Ð°Ð¿ÑÐ°Ð²Ð¸ÑÑ Ð½Ð° ÑÐ°Ð±Ð¾ÑÑ, Ð½Ð°Ð¿ÑÐ¸Ð¼ÐµÑ, Ð¿Ð¾Ð»ÐµÐ·Ð½Ð¾Ð¹ Ð½Ð°Ð³ÑÑÐ·ÐºÐ¸.
description: The object of the study is a thermal management system. The purpose of the work is to study and improve the TMS for the most vulnerable electronics unit in the small spacecraft of the CubeSat nanoclass format. During the study, the following tasks were performed: â to consider which main blocks of equipment and on-board systems the SS of the nanoclass consists of; â to consider the problems of development and possible problems of power supply of the main units of the SS nanoclass equipment; â to study the features of the application of the SS of the nanoclass, as well as to consider the design and layout scheme of the current SS nanoclass like a Polytech Universeâ3 (next â PUâ3); â to consider various types and actual implementations of the TMS electronics of domestic and foreign SS of the nanoclass; â consider the TMS in the current SS PUâ3; â to conduct an experimental study of the effectiveness of the TMS of the most vulnerable unit of the SS PUâ3 equipment; â based on the data obtained, make recommendations on the implementation of an effective TMS. The result of the study are proposals for improving TMS in the current SS PU-3. It is proposed to use screen-vacuum thermal insulation, as well as implement a power supply system in such a way as to achieve thermal stabilization of the battery block, and direct the saved energy to work, for example, a payload.