FIELD: transport.
SUBSTANCE: invention relates to aerospace engineering and may be used for programmable displacement of coordinates of spacecraft separation stages fall points. Rocket gas engine and separation stages control program is divided into extra-atmospheric and atmospheric sections. Said sections are divided into finite number of time intervals to define the program of separation stage angular turn and motion at every said interval.
EFFECT: complete combustion of liquid propellant components, varying and lowering fall points.
2 cl, 2 dwg
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