RESEARCH AND DEVELOPMENT OF NEW VERSION OF A LIFT-OFF SEAL OF OXIDIZER PUMP




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RESEARCH AND DEVELOPMENT OF NEW VERSION OF A LIFT-OFF SEAL OF OXIDIZER PUMP

OF RD191 ENGINE
Results of calculation and design works on experimental lift-off seal operating at high pressure drop and designed to sealing liquid oxygen in oxidizer pump presents are presented in article. Results of autonomous tests proving operability of seal at conditions close to operational ones are presented. Comparison of characteristics of experimental variants with base lift-off seal of RD191 engine, confirmed high efficiency of experimental seal is conducted.

Keywords: liquid rocket engine, turbopump unit, lift-off seal, test.
Literature

UDC 621.45:519.87


Gromyko Boris Mikhailovich, doctor of tech.sciences.

Krapivnykh Elena Vladimirovna.

Telenkov Alexander Alekseevich, cand. of tech.sciences/

Tyurin Alexander Anatolievich.

Russia, Moscow region, Khimki, NPO Energomash named after academician V.P. Glushko. Tel. (495) 286-92-54.

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RESEARCH AND DEVELOPMENT OF NEW VERSION OF A LIFT-OFF SEAL OF OXIDIZER PUMP

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