SOLID PROPELLANT CHARGE FOR DUAL THRUST ROCKET ENGINE Russian patent published in 1999 - IPC

Abstract RU 2131053 C1

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

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RU 2 131 053 C1

Authors

Dubinin V.A.

Lugovoj A.N.

Aksenenko D.D.

Mar'Jash V.I.

Romanov E.P.

Zharkov A.S.

Dates

1999-05-27—Published

1996-08-15—Filed