A Rocket Engine With Integrated Combustor Head And Turbopump

The present invention relates to a rocket engine with integrated combustor head and turbopump, wherein the turbopump and the combustor head of the rocket engine are integrated. The disclosed rocket engine with the integrated combustor head and turbopump includes an oxidant supply pipe through which...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	LEE KEUM OH, LIM BYOUNGJIK, KIM CHEULWOONG
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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