Abstract
Heat stores of different design are compared, with a view to identifying the maximum stored energy density and power [1, 2]. The heat store selected has a melting working medium. This design is the most promising for the maintenance of acceptable thermal conditions in spacecraft [3, 4].
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REFERENCES
Borshev, N.O., Sorokin, A.E., and Belyavskii, A.E., Mutual influence of capillary pumps in heat-pipe systems with different evaporator loads, Russ. Eng. Res., 2019, vol. 39, no. 9, pp. 782–784.
Kudryavtseva, N.S., Sadretdinova, E.R., and Zagovorchev, V.A., Solar hot water system for a habitable base at the poles of the Moon, Al’tern. Energ. Ekol., 2019, nos. 7–9 (291–293), pp. 85–96.
Belyavskii, A.E., Novikov, S.V., Sorokin, A.E., and Shangin, I.A., Thermal stores in spacecraft heating systems, Russ. Eng. Res., 2019, vol. 39, no. 6, pp. 507–509.
Strogonova, L.B., Sorokin, A.E., Vasin, Yu.A., and Belyavskii, A.E., Creating an atmosphere within spacecraft, Russ. Eng. Res., 2019, vol. 39, no. 9, pp. 813–815.
Kudryavtseva, N.S., Indicators of reliability and equivalent mass of life support systems for flights into deep space, Aviakosm. Ekol. Med., 2019, vol. 53, no. 3, pp. 5–12.
Borshchev, N.O., Sorokin, A.E., and Belyavskii, A.E., Thermophysical characteristics of isotropic coatings on a spacecraft in Earth orbit, Russ. Eng. Res., 2020, vol. 40, no. 2, pp. 171–174.
Borshchev, N.O., Sorokin, A.E., and Belyavskii, A.E., External heating of spacecraft, Russ. Eng. Res., 2020, vol. 40, no. 2, pp. 168–170.
Belyavskii, A.E. and Shangin, I.A., The efficiency of joint operation of the heat accumulator and the emitter radiator in the supporting systems of the thermal regime of spacecrafts, Materialy 17-oi mezhdunarodnoi konferentsii “Aviatsiya i kosmonavtika,” Moskva, 19–23 noyabrya 2018 g. (Proc. 17th Int. Conf. “Aviation and Cosmonautics,” Moscow, November 19–23, 2018), Moscow: Mosk. Aviats. Inst., 2018.
Borshchev, N.O., Sorokin, A.E., and Belyavskii, A.E., Heat pipe with a thermal hydraulic store, Russ. Eng. Res., 2020, vol. 40, no. 2, pp. 175–178.
Borshchev, N.O. and Belyavskii, A.E., Analytical dependencies for calculation of the limiting cases of determination of the minimum design parameters of the radiator with maximum emissivity, Materialy Sed’moi Rossiiskoi natsional’noi konferentsii po teploobmenu, Moskva, 22–26 oktyabrya 2018 g. (Proc. Seventh Russian National Conf. on Heat Exchange, Moscow, October 22–26, 2018), Moscow: Mosk. Energ. Inst., 2018.
Zagovorchev, V.A. and Tushavina, O.V., The use of jet penetrators for movement in the lunar soil, INCAS Bull., 2019, vol. 11, pp. 121–130.
Zagovorchev, V.A. and Tushavina, O.V., Selection of temperature and power parameters for multi-modular lunar jet penetrator, INCAS Bull., 2019, vol. 11, special issue, pp. 231–241.
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Translated by B. Gilbert
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Belyavskii, A.E. Heat Stores with a Melting Working Medium for Spacecraft Thermal Control Systems. Russ. Engin. Res. 41, 56–57 (2021). https://doi.org/10.3103/S1068798X21010044
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DOI: https://doi.org/10.3103/S1068798X21010044