Article

Cover

Title

Improvement units for transporting heat in a spacecraft

Authors

¹V.V. Dvirnyi, ^2,3G.G. Krushenko, ⁴V.V. Golovanova, ¹G.V. Dvirnyi, ¹N.N. Petyaeva, ¹K.A. Kiryanova

Organizations

¹JCS «Academician M. F. Reshetnev» Information Satellite Systems»
Zheleznogorsk, Russian Federation
²Institute Computational Modeling SB RAS
Krasnoyarsk, Russian Federation
³Reshetnev Siberian State Aerospace University
Krasnoyarsk, Russian Federation
⁴The Arsenal Design Bureau named after M. V. Frunze
Saint-Petersburg, Russian Federation

Abstract

This paper covers creation period of units for transporting heat in a spacecraft from the 70-s of the last century to the present time. In the development of space technology communication, navigation and geodesy were created numerous types of spacecrafts with various types of thermal control systems and units for transporting heat while the general trend of increasing power consumption and heat dissipation, increasing the number of thermal couplings and improve the efficiency of heat distribution, increasing active shelf life up to 15 years. The appearance of modern spacecraft largely determines the choice of thermal systems and units for transporting heat and in the case of containerless option when developing a block-modular spacecraft structure, honeycomb and topology of the heat pipes are fundamental, requiring solutions of complex applied thermal problems. Also this paper covers the problem of multiple heat flows transmission and distribution, which solve the units for transporting heat, while providing the required range of gas temperature in a sealed container. This paper presents long life ensure of low consumption blowers in a spacecraft of units for transporting heat liquid in service, as a solution of the most scienceintensive task for the rapidly rotating rotor of electric pump units.

Keywords

transporting heat, spacecrafts, heat pipes, gas-controlled heat pipes, thermal control system, electric pump unit, low consumption fan

References

[1] David G. Gilmore. Fundamental Technologies. Spacecraft Thermal Control Handbook, 2002. Vol. I. 836 р.

[2] Dvirnyi V. V., Kraev M. V. low consumption self-contained blowers. Krasnoyarsk: Univ Publ., 1985. 152 с.

[3] Golovenkin E. N., Dvirnyj V. V., Kovalev N. А., Kraev M. V. pod red. K. G. Smirnova-Vasil'eva, Аgregaty avtonomnykh ehnergeticheskikh system [Units of self-contained power systems]. Krasnoyarsk: KrPi., Publ., 1986. 89 с.

[4] Dvirnyj V. V. Theory and practice of units for transporting heatin the spacecraft with a long active life. Materialy Mezhdunarodnoj nauchno-tekhnicheskoj konferentsii «Problemy obespecheniya kachestva izdelij v mashinostroenii» [Problems of maintenance of product quality inmechanical engineering]. KGPU. Krasnoyarsk, 1994. P. 402–406. (In Russ.)

[5] Chajkina I., Karmakova M., Shherbakova Y. «Express AM8» – a new satellite for the Russian orbital group] // Sibirskiy sputnik. 2015. Vol. 16, N. 4. P. 1. (In Russ.)

[6] Chajkina I., Karmakova M., Shherbakova Y. Promptly, and without comment // Sibirskiy sputnik. 2015. Vol. 19, No. 18. P. 1. (In Russ.)

[7] Testoedov N. А., Dvirnyi G. V., Turkenich R. P. Evaporation-condensation device for use in robotics and space technology. Materialy II nauchno-prakticheskoj konferentsii ‘Robototekhnika kak obrazovatel'naya tekhnologiya’ [Robotics as an educational technology]. Filial SFU, Zheleznogorsk, 2011. P. 49. (In Russ.)

[8] Testoedov N. А., Dvirnyj G. V., Golovanova V. V. [Space technologies of heat transporting units with change of unit state]. Trudy Х nauchno-prakticheskoj konferentsii «Intellektinauka» [Intelligence and science]. Filial SFU, Zheleznogorsk, 28–29 th April, 2011. P. 3–6 (In Russ.).

[9] Dvirnyj V. V., Smirnov-Vasil'ev K. G., Panov G. I., Ovechkin G. I. [Modeling of heat pipes characteristics in the calculation of non-stationary temperature field structure with heat pipes]. Materialy Mezhdunarodnoj nauchnotekhnicheskoj konferentsii «Problemy obespecheniya kachestva izdelij v mashinostroenii» [Problems of maintenance of product quality in mechanical engineering]. KGPU. Krasnoyarsk, 1994. P. 462–468. (In Russ.)

[10] Dvirnyj V. V., Majdanik YU. F., Pastukhov V. G. [Development of analytical and experimental studies of loop heat pipes]. Materialy 7 Mezhdunarodnoj nauchnoj konferentsii ‘teplovie trubi’ [Heat pipes]. Institut teplomassoobmena im. А. V. Lykova, Minsk, 1990. P. 55–59. (In Russ.)

[11] Krushenko G. G., Golovanova V. V. [Balancing ofsome spacecraft units]. Vestnik SibGАU. 2014. N. 3. P. 178–184. (In Russ.)

For citing this article

Dvirnyi V.V., Krushenko G.G., Golovanova V.V., Dvirnyi G.V., Petyaeva N.N., Kiryanova K.A. Improvement units for transporting heat in a spacecraft // The Research of the Science City, 2016, no. 3-4, pp. 12-16.

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