Head pressure enhancement of rotary and disk pumps for flying vehicles

Аuthors

Ovsiannikov B. V.¹, Shapiro A. S.², Bobkov A. V.³, Zhdanov I. L.¹

1. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
2. Isayev chemical design engineering bureau branch Khrunichev State Research and Production Space Center, 12, Bogomolov st., Korolev, Moscow region, 141070, Russia
3. Komsomolsk-na-Amure State University, 27, Lenina str., Komsomolsk-on-Amur, 681013, Russia

Abstract

A problem of head pressure enhancement for rotary and disk pumps is very important for design of aerospace vehicle fuel systems. Theoretical abd experimental investigation is carried out to solve this problem. Main results obtained is analysed and discussed.