Results of Ground-Based Testing of Passive Heat Protection for Liquid Helium Temperature Spacecraft Devices


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The paper presents the results of thermal vacuum testing of space technology components and instruments using local helium cryo-panels (“shrouds”) in a liquid nitrogen thermal vacuum chamber. A structural description of prototypes and upgraded helium shrouds is given. The results of experimental layouts at the helium temperature level are presented.

作者简介

A. Vshivkov

Reshetnev Siberian State University of Science and Technology (Reshetnev University)

Email: lavrovna@bmstu.ru
俄罗斯联邦, Krasnoyarsk

A. Delkov

Reshetnev Siberian State University of Science and Technology (Reshetnev University)

Email: lavrovna@bmstu.ru
俄罗斯联邦, Krasnoyarsk

A. Kishkin

Reshetnev Siberian State University of Science and Technology (Reshetnev University)

Email: lavrovna@bmstu.ru
俄罗斯联邦, Krasnoyarsk

N. Lavrov

Bauman Moscow State Technical University

编辑信件的主要联系方式.
Email: lavrovna@bmstu.ru
俄罗斯联邦, Moscow

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