SOLID-PROPELLANT CHARGE IGNITER

rocketry. SUBSTANCE: proposed igniter consists of weight amount of igniting composition arranged in hermetically sealed envelope. Envelope of two-layer design consists of synthetic polymeric films of different melting points. Melting point of inner layer of envelope. Envelope can be made in form of...

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Bibliographische Detailangaben
Hauptverfasser:	CHURAKOV V.V, KOLESNIKOV V.I, MEL'NICHENKO M.V, MOLCHANOV V.F, KOZ"JAKOV A.V, KUZ'MITSKIJ G.EH, PUPIN N.A
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:	rocketry. SUBSTANCE: proposed igniter consists of weight amount of igniting composition arranged in hermetically sealed envelope. Envelope of two-layer design consists of synthetic polymeric films of different melting points. Melting point of inner layer of envelope. Envelope can be made in form of rectangular pack divided by cross bridges into sections which are arranged in bellows-like manner. Cross bridges can be interrupted. EFFECT: provision of highly effective hermetically0sealed igniter of excellent performance. 9 cl, 7 dwg