Open AccessMethod of calculating the thickness of the combustion chamber of a liquid rocket engine made with the use of innovative technologies and materials
Author(s) -
А. В. Кривоногов
Publication year - 2016
Publication title -
vestnik samarskogo universiteta. aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie
Language(s) - English
Resource type - Journals
eISSN - 2541-7533
pISSN - 2542-0453
DOI - 10.18287/2541-7533-2016-15-4-81-90
Subject(s) - combustion chamber , propellant , nozzle , combustion , mechanical engineering , chamber pressure , liquid propellant rocket , thermal conduction , jet (fluid) , rocket engine , aerospace engineering , jet engine , rocket (weapon) , mechanics , materials science , flow (mathematics) , nuclear engineering , engineering , physics , composite material , chemistry , organic chemistry