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

  • A. Yu. Vshivkov
  • A. V. Delkov
  • A. A. Kishkin
  • N. A. LavrovEmail author
Article

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.

Keywords

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

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Copyright information

© Springer Science+Business Media, LLC, part of Springer Nature 2019

Authors and Affiliations

  • A. Yu. Vshivkov
    • 1
  • A. V. Delkov
    • 1
  • A. A. Kishkin
    • 1
  • N. A. Lavrov
    • 2
    Email author
  1. 1.Reshetnev Siberian State University of Science and Technology (Reshetnev University)KrasnoyarskRussia
  2. 2.Bauman Moscow State Technical UniversityMoscowRussia

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