METHOD OF DETERMINING MANEUVER TERMINATION INTERVAL AND SHUTTING DOWN OF ACCELERATION UNIT SUSTAINER ENGINE

FIELD: transport.SUBSTANCE: invention relates to termination control of rocket acceleration unit uncontrolled-thrust sustainer engines. Proposed method comprises forecasting sustainer engine shutdown in changing over to termination control before spaceship separation when functional reaches preset p...

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Hauptverfasser:	SOKOLOV VLADIMIR NIKOLAEVICH, MISHCHIKHIN VJACHESLAV VITAL'EVICH, EZHOV VLADIMIR VASIL'EVICH, BOCHAROV MIKHAIL VIKTOROVICH, SYROV ANATOLIJ SERGEEVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR
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