ROCKET ENGINE WITH INTEGRATED COMBUSTOR HEAD AND TURBOPUMP

The present disclosure relates to a rocket engine, and more particularly, a rocket engine with an integrated combustor head and turbopump in which a turbopump of the rocket engine is formed integrally with a combustor head.

Bibliographische Detailangaben

Hauptverfasser:	LEE, Keum-Oh, LIM, Byoungjik, KIM, Cheulwoong
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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