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...

Ausführliche Beschreibung

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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