Open AccessAutomated thermovacuum firing test facility for testing and research of workflow in low-thrust rocket engine on hypergolic propellants
Author(s) -
Р. Н. Гальперин,
Ю. С. Ивашин,
В. Е. Нигодюк,
В. В. Рыжков,
А. В. Сулинов
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 - 10.18287/1998-6629-2014-0-5-2(47)-48-58
Subject(s) - thrust , propellant , aerospace engineering , rocket engine , jet engine , jet (fluid) , mechanical engineering , liquid propellant rocket , nuclear engineering , automotive engineering , environmental science , engineering