Improvement of power characteristics of liquid-propellant rockets by means of automatic control. Part Ii: physicotechnical bases of fuel consumption control
Abstract:
The basic results of semicentenial development of family of control systems of liquid fuel consumption for
domestic carrier rockets and intercontinental ballistic missiles are stated. Physicotechnical bases of construction of these systems are explained.
Keywords:liquid rocket engines, power characteristics, guarantee fuel capacity, management of fuel consumption.
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