ANALYSIS OF HEAT-EXCHANGING DEVICE APPLICATION IN LIQUID PROPELLANT JET ENGINES
One of the tasks of space rocket hardware heat-exchangers is to provide and maintain the temperature level required for trouble-free operation of all elements of flying vehicles. A characteristic feature of all heat sources is the inconstancy of transmitted heat. The integrity of rocket engines and aircraft as a whole depends on the solution of this problem, so the article deals with the design of heat-exchange apparatuses for liquid rocket propulsion systems, their purpose, classification, advantages and disadvantages.