METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH CLOSED STEAM-LIQUID CONTOUR IN TURBOPUMP DELIVERY SYSTEM

METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH CLOSED STEAM-LIQUID CONTOUR IN TURBOPUMP DELIVERY SYSTEM

FIELD: rocket engines. SUBSTANCE: according to proposed method working steam for operation of turbine is obtained from water using heat of rocket propellant combustion products. Steam is operated to pressure of 0.6-4.0 MPa. Used steam is cooled using cold of oxidizer and condensate is returned into...

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Bibliographische Detailangaben
Hauptverfasser: MIROSHKIN V.V, PRISHCHEPA V.I, BUKANOV V.T, KLEPIKOV I.A
Format: Patent
Sprache:eng ; rus
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Beschreibung
Zusammenfassung:FIELD: rocket engines. SUBSTANCE: according to proposed method working steam for operation of turbine is obtained from water using heat of rocket propellant combustion products. Steam is operated to pressure of 0.6-4.0 MPa. Used steam is cooled using cold of oxidizer and condensate is returned into water pump. EFFECT: prevention of freezing of water condensate at high pressure level in chamber. 2 dwg