z-logo
open-access-imgOpen Access
Results of experimental studies of parameters of low-thrust rocket engines operating on gaseous oxygen-hydrogen fuel
Author(s) -
Ю. И. Агеенко,
Евгений Александрович Лапшин,
И. И. Морозов,
И. В. Пегин,
В. В. Рыжков
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 - 10.18287/1998-6629-2014-0-5-3(47)-35-45
Subject(s) - specific impulse , combustion chamber , rocket engine , thrust , ignition system , combustion , rocket (weapon) , nozzle , rocket engine nozzle , nuclear engineering , aerospace engineering , mechanical engineering , materials science , chemistry , engineering , organic chemistry

The content you want is available to Zendy users.

Already have an account? Click here to sign in.
Having issues? You can contact us here