Open AccessOxygen-hidrogen liquid rocket engine using turbo-pump developed for aviation hidrogen liquid two-spool turbo-jet
Author(s) -
Александр Иванович Иванов,
В. А. Борисов
Publication year - 2014
Publication title -
vestnik samarskogo universiteta. aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie
Language(s) - English
Resource type - Journals
eISSN - 2541-7533
pISSN - 2542-0453
DOI - 10.18287/2541-7533-2012-0-3-2(34)-302-306
Subject(s) - rocket engine , turbo , liquid propellant rocket , liquid hydrogen , liquid oxygen , rocket (weapon) , aerospace engineering , nuclear engineering , aviation , turbine , jet engine , gas turbines , aeronautics , hydrogen , engineering , oxygen , automotive engineering , physics , mechanical engineering , propellant , quantum mechanics
The possibility of using in small trust rocket engines hydrogen turbopump unit developed for aircraft gas turbine engine is considered.