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

被引：9

作者：

Vshivkov, A. Yu. ^{[1
]}

Delkov, A. V. ^{[1
]}

Kishkin, A. A. ^{[1
]}

Lavrov, N. A. ^{[2
]}

机构：

[1] Reshetnev Univ, Reshetnev Siberian State Univ Sci & Technol, Krasnoyarsk, Russia

[2] Bauman Moscow State Tech Univ, Moscow, Russia

来源：

CHEMICAL AND PETROLEUM ENGINEERING | 2019年 / 55卷 / 3-4期

关键词：

liquid nitrogen thermal vacuum chamber; liquid helium; thermal vacuum tests; prototype; spacecraft;

D O I：

10.1007/s10556-019-00619-4

中图分类号：

TQ [化学工业];

学科分类号：

0817 ;

摘要：

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.

引用

页码：306 / 311

页数：6

共 9 条

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[3] Kolesnikov A. V., 2007, SUMMARY LECT COURSE
[4] Krat S. A., 2010, VESTNIK SIB GAU, V4, P123
[5] Kravchenko S. V., 2013, INZHENERNYJ ZH NAUKA, V1, P149
[6] Malkov M.P, 1985, Handbook on the physical and technical foundations of cryogenics
[7] Solntsev Yu. P., 1982, Materials in Cryogenic Technology: Handbook in Russian
[8] Vshivkov A. Yu, 2018, KHIM NEFTEGAZ MASHIN, P30
[9] Zolotovskaya S. V., 1991, HELIUM CRYOSTATS SCI

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