Chayka D. Stationary air temperature control system of space rocket complex for operating in the tropical climate

The object is a temperature and humidity controlling for space missile system during the prelaunch preparation; The aims is a improving the characteristics of stationary air thermal control system for space missile system to ensure effective operation in a wet tropical climate; methods - physical modeling, mathematical modeling, analysis and synthesis of complex technical systems, variance and regression analysis, mathematical and statistic processing of experiments;novelty - the improved concept of temperature control system, which designed to operating in the tropical climate is proposed; the empirical relationship which quantitatively describes the condensate effect and other heat transfer factors in plate heat exchangers in the range as a humid tropical climate is first time obtained; calculation method for operating parameters of the temperature control systems, based on the mathematical model of nonstationary hydraulic processes that take into account the condensation effects in plate heat exchangers was further developed; correlation parameters of the mathematical model of thermal control system was obtained; results - thermal control systems development, quality improvement of project activities; industry - aircraft and rocket.