TURBO-PUMP SUPPLY SYSTEM FOR LIQUID-PROPELLANT ROCKET ENGINE

FIELD: liquid-propellant rocket engines. ^ SUBSTANCE: proposed system includes lines of different propellant components, gas lines and gas generator. Mounted in front of main turbo-pump unit with multi-stage propellant component pump and drive gas turbine is booster turbo-pump unit with propellant c...

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Bibliographische Detailangaben
Hauptverfasser:	MIROSHKIN V.V, KANALIN JU.I, PRISHCHEPA V.I, BAKHMUTOV A.A, 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: liquid-propellant rocket engines. ^ SUBSTANCE: proposed system includes lines of different propellant components, gas lines and gas generator. Mounted in front of main turbo-pump unit with multi-stage propellant component pump and drive gas turbine is booster turbo-pump unit with propellant component pump and drive single-stage hydraulic turbine fed from "n" stage of main pump. Working passage of hydraulic turbine is located in connecting line between outlet of "n" stage and inlet of "(n+1)" stage of main pump. ^ EFFECT: simplified construction; reduced mass of liquid propellant. ^ 3 cl, 1 dwg