TRUMPET OF NOZZLE OF ROCKET ENGINE WITH HEAT-FLOW BARRIER

FIELD: rocket technics.SUBSTANCE: invention relates to rocket engineering. Trumpet nozzle of rocket engine with heat insulation is made from composite material that is represented by ceramic matrix which is reinforced with carbon fibers. Heat insulation is made in the form of housing from the packet...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Ulyanova Marina Viktorovna, Volkov Nikolaj Nikolaevich, Davydenko Nikolaj Andreevich, TSatsuev Sergej Mikhajlovich, Volkova Larisa Ivanovna
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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