SOLID PROPELLANT CHARGE FOR DUAL THRUST ROCKET ENGINE

FIELD: rocket engine; provision of stepped changing of engine thrust. SUBSTANCE: charge has splitter plate between its parts which is made in form of gasless burning grain. This provides reliable cutoff of thrust for preset time interval without complicating the design of charge and introducing spec...

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Bibliographische Detailangaben
Hauptverfasser:	AKSENENKO D.D, MAR'JASH V.I, ZHARKOV A.S, DUBININ V.A, LUGOVOJ A.N, ROMANOV E.P
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	FIELD: rocket engine; provision of stepped changing of engine thrust. SUBSTANCE: charge has splitter plate between its parts which is made in form of gasless burning grain. This provides reliable cutoff of thrust for preset time interval without complicating the design of charge and introducing special design members into engine. EFFECT: enhanced reliability of engine. 1 dwg