Single-chamber double-thrust solid rocket engine with high thrust ratio

The invention discloses a single-chamber double-thrust solid rocket engine with a high thrust ratio. The single-chamber double-thrust solid rocket engine at least comprises a charging combustion chamber, a spray pipe, an ignition device and a throat adjusting mechanism. The charging combustion chamb...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	TANG HAO, JIN WEI, ZHENG CAILANG, LAI MOURONG, LIU YONGKANG
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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