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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Authors
Dates
1999-07-27—Published
1996-11-04—Filed