Some aspects of the simulation of temperature control systems for space vehicles

1Makarova, AS, 1Ivanova, GA, 1Zavelion, VI
1Oles Honchar National University of Dnipropetrovsk, Dnipropetrovsk, Ukraine
Kosm. nauka tehnol. 1998, 4 ;(1):90–91
Section: Space Energy, Power and Propulsion
Publication Language: Russian
We discuss the essential features required of the general mathematical models for calculating temperature control systems. The most promising models showed combine engineering methods and boundary-valued problems formulated for partial differential equations.
Keywords: combine methods, space energy, temperature control systems
1.  Dul’nev G. N., Parfenov V. G., Sigalov A. V. Methods of Calculating the Device Thermal Mode [Metody rascheta teplovogo rezhima priborov], 312 p. (Radio i Svyaz’, Moscow, 1990) [in Russian].

2.  Malozemov V. V. The Thermal Regime of Spacecraft [Teplovoj rezhim kosmicheskih apparatov], 367 p. (Mashinostroenie, Moscow, 1980) [in Russian].