IGNITION DEVICE FOR ROCKET PROPELLANTS Russian patent published in 1999 - IPC

Abstract RU 2133725 C1

FIELD: devices intended for ignition of rocket propellants in solid-propellant rocket engines and other power plants. SUBSTANCE: ignition device consists of a body and charge made of igniting composition with catalyst of solid-propellant combustion in correlation within 95/5 to 55/45 by mass. EFFECT: provision of low values of time parameters for engine to get into the rated duty and reduced thermal loads on the charge and members of the engine combustion chamber. 2 dwg, 2 tbl

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RU 2 133 725 C1

Authors

Sarab'Ev V.I.

Emel'Janov V.N.

Levina N.A.

Kinevskij P.B.

Dates

1999-07-27Published

1996-11-04Filed