Analysis of the systems for ensuring thermal regimes of domestic spacecraft
Authors: Borschev N.O., Belyavsky A.E., Antonov V.A.
Published in issue: #7(127)/2022
DOI: 10.18698/2308-6033-2022-7-2193
Category: Aviation and Rocket-Space Engineering | Chapter: Design, construction and production of aircraft
Along with the designing configuration of spacecraft for various purposes, in parallel, the choice of the configuration and location of the systems ensuring thermal regime takes place. In such systems, in addition to the construction itself, depending on the target orbit and heat-generating equipment a huge number of different elements can be included, ensuring equipment temperature control and, if it is a manned spacecraft ensuring also the necessary requirements for maintaining a constant temperature and humidity in the pressurized compartment. Therefore, this article discusses autonomous elements of active and passive domestic thermal management systems currently used in the design of non-pressurized spacecraft. This will help in making the most correct technical solution when developing a spacecraft in terms of cost, reliability, durability and normal operation of the target onboard equipment.
References
[1] Fleyshman G.D. Stokhasticheskaya teoriya izlucheniya [Stochastic theory of radiation]. Moscow, Mashinostroenie Publ., 2008, pp. 202–230.
[2] Bloch A.G., Zhuravlev Yu.A., Ryzhkov L.N. Teploobmen izlucheniyem [Heat transfer by radiation]. Moscow, Energoatomizdat Publ., 1991, pp. 10–50.
[3] Zaletaev V.M., Kapinos Yu.V., Surguchev O.V. Raschet teploobmena kosmicheskogo apparata [Spacecraft heat transfer calculation]. Moscow, Mashinostroenie Publ., 1979, 208 p.
[4] Favorsky O.N., Kadaner Ya.S. Voprosy teploobmena v kosmose [Problems of heat transfer in space]. Moscow, Vysshaya shkola Publ., 1967, pp. 68–73.
[5] Alekseev S.V., Aksenova I.V., Belokrylova V.V., Ivanova E.K., Kolesnikova E.N., Kharitonova E.V. Vestnik «NPO imeni S.A. Lavochkina» — Space Journal of ”Lavochkin Association, JSC”. Cosmonautics and Rocket Engineering, 2015, no. 4 (30), pp. 65–69.
[6] Efanov V.V., Martynov M.B., Karchaev H.Zh. Vestnik «NPO imeni S.A. Lavochkina» — Space Journal of ”Lavochkin Association, JSC”. Cosmonautics and Rocket Engineering, 2017, no. 2/36, pp. 5–16.
[7] Aksamentov V.A., Bednov S.M., Zaletayev S.V., Zelenov I.A., Kopyatkevich R.M., Malozemov V.V., Mishin G.S., Novikov S.B., Tarasov A.R., Surguchev O.V. Rukovodstvo dlya konstruktorov po obespecheniyu teplovykh rezhimov. Tom 1. Raschet vneshnikh teplovykh nagruzok i luchistogo teploobmena KA [A guide for designers to ensure thermal conditions. Vol. 1. Calculation of external thermal loads and spacecraft radiant heat transfer]. Kaliningrad, GONTI Publ., 1992, 131 p.
[8] Altov V.V., Zaletaev S.V., Kopyatkevich R.M. Kosmonavtika i raketostroenie — Cosmonautics and Rocket Engineering, 2005, no. 2 (39). pp. 18–22.
[9] Selivanov A.S. Vestnik «NPO imeni S.A. Lavochkina» — Space Journal of “Lavochkin Association, JSC”. Cosmonautics and Rocket Engineering, 2012, no. 4 (15), pp. 127–134.
[10] Tulin D.V., Finchenko V.S. Teoretiko-eksperimentalnyye metody proyektirovaniya sistem obespecheniya teplovogo rezhima kosmicheskikh apparatov. V 3 tomakh. T. 3 Proyektirovaniye avtomaticheskikh kosmicheskikh apparatov dlya fundamentalnykh nauchnykh issledovaniy [Theoretical and experimental methods for designing systems for ensuring the spacecraft thermal regime. In 3 vols. Vol. 3. Design of automatic space vehicles for fundamental scientific research]. Moscow, MAI PRINT Publ., 2014, vol. 3, pp. 1320–1437.
[11] Anfimov N.A., Altov V.V., Zaletaev S.V., Kopyatkevich P.M. Konversiya v mashinostroyenii — Conversion in machine building of Russia, 2007, no. 1, pp. 19–23.
[12] Khartov V.V., Vestnik «NPO imeni S.A. Lavochkina» — Space Journal of “Lavochkin Association, JSC”. Cosmonautics and Rocket Engineering, 2011, no. 3, pp. 3–10.
[13] Malozemov V.V., Kudryavtseva N.S. Sistemy termoregulirovaniya kosmicheskikh apparatov [Thermal control systems for spacecraft]. Moscow, Mashinostroenie Publ., 1995, 112 p.
[14] Malozemov V.V., Rozhnov V.F., Pravetsky V.N. Sistemy zhizneobespecheniya ekipazhey letatelnykh apparatov [Space crew life support systems]. Moscow, Mashinostroenie Publ., 1986, 584 p.
[15] Tsaplin S.V., Bolychev S.A., Romanov A.E. Teploobmen v kosmose [Heat transfer in space]. Samara, Samara University Publ., 2013, 53 p.
[16] Chi S.W Heat Pipe Theory and Practice: A Sourcebook. Washington, D.C., Hemisphere Publishing Corp. Publ.; New York, McGraw-Hill Book Co. Publ., 1976, 256 p. [In Russ.: Chi S.W. Teplovyye truby: teoriya i praktika. Moscow, Mashinostroenie Publ., 1981, 207 p.].