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

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Chemical and Petroleum Engineering Aims and scope

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.

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References

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Authors and Affiliations

  1. Reshetnev Siberian State University of Science and Technology (Reshetnev University), Krasnoyarsk, Russia

    A. Yu. Vshivkov, A. V. Delkov & A. A. Kishkin

  2. Bauman Moscow State Technical University, Moscow, Russia

    N. A. Lavrov

Authors
  1. A. Yu. Vshivkov
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  2. A. V. Delkov
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  3. A. A. Kishkin
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  4. N. A. Lavrov
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Corresponding author

Correspondence to N. A. Lavrov.

Additional information

Translated from Khimicheskoe i Neftegazovoe Mashinostroenie, Vol. 55, No. 4, pp. 25–28, April, 2019.

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Vshivkov, A.Y., Delkov, A.V., Kishkin, A.A. et al. Results of Ground-Based Testing of Passive Heat Protection for Liquid Helium Temperature Spacecraft Devices. Chem Petrol Eng 55, 306–311 (2019). https://doi.org/10.1007/s10556-019-00619-4

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  • DOI: https://doi.org/10.1007/s10556-019-00619-4

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