SOLID-PROPELLANT ROCKET ENGINE Russian patent published in 1998 - IPC

Abstract RU 2118686 C1

FIELD: total thrust pulse control in rocket engineering. SUBSTANCE: engine has case 1 accommodating main charge 2, main nozzle 3 whose bell mouth mounts droppable thrust-level variation unit 4. Case mounts for radial displacement droppable gas generators 6 held in position by means of explosive lock 7. Inner spaces of gas generators communicate with case space either directly or through shut-off valve separating them. EFFECT: improved precision of control and operating reliability of engine. 1 dwg

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RU 2 118 686 C1

Authors

Ljanguzov S.V.

Dates

1998-09-10—Published

1996-09-11—Filed