Results of Ground-Based Testing of Passive Heat Protection for Liquid Helium Temperature Spacecraft Devices
- Authors: Vshivkov A.Y.1, Delkov A.V.1, Kishkin A.A.1, Lavrov N.A.2
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Affiliations:
- Reshetnev Siberian State University of Science and Technology (Reshetnev University)
- Bauman Moscow State Technical University
- Issue: Vol 55, No 3-4 (2019)
- Pages: 306-311
- Section: Article
- URL: https://ogarev-online.ru/0009-2355/article/view/236553
- DOI: https://doi.org/10.1007/s10556-019-00619-4
- ID: 236553
Cite item
Abstract
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.
About the authors
A. Yu. Vshivkov
Reshetnev Siberian State University of Science and Technology (Reshetnev University)
Email: lavrovna@bmstu.ru
Russian Federation, Krasnoyarsk
A. V. Delkov
Reshetnev Siberian State University of Science and Technology (Reshetnev University)
Email: lavrovna@bmstu.ru
Russian Federation, Krasnoyarsk
A. A. Kishkin
Reshetnev Siberian State University of Science and Technology (Reshetnev University)
Email: lavrovna@bmstu.ru
Russian Federation, Krasnoyarsk
N. A. Lavrov
Bauman Moscow State Technical University
Author for correspondence.
Email: lavrovna@bmstu.ru
Russian Federation, Moscow
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