Two-component variable-thrust rotary detonation rocket engine based on pintle injector

The invention discloses a two-component variable-thrust rotary detonation rocket engine based on a pintle injector. The two-component variable-thrust rotary detonation rocket engine based on the pintle injector comprises the pintle injector, a rotary detonation combustion chamber and an exhaust nozz...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LIN WEI, YAN CHENGLONG, SHI QIANG, WANG JIASEN, LUO XIUQI, FAN LIANGZHONG, SU LINGYU, ZHAO JIAFENG, GUO KANGKANG
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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