OXIDISER TURBOPUMP UNIT FOR GENERATOR-FREE LIQUID-PROPELLANT ROCKET ENGINE

FIELD: engines and pumps.SUBSTANCE: proposed turbopump unit comprises oxidiser pump, turbine running on gas fuel, turbine bearing, system of seals separating said oxidiser pump from said turbine. Gas drainage between the system of seals and turbine, seal being fitted on turbine side Turbine bearing...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KRAVCHENKO ANATOLIJ GEORGIEVICH, DEM'JANENKO JURIJ VASIL'EVICH, GLUSHKO IGOR' NIKOLAEVICH, DMITRENKO ANATOLIJ IVANOVICH, IVANOV ANDREJ VLADIMIROVICH
Format:	Patent
Sprache:	eng ; rus
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!