
Research of the influence of design parameters of a 400 N-thrust low-thrust liquid rocket engine on its energy efficiency
Author(s) -
Ю. И. Агеенко,
Р. В. Ильин,
И. В. Пегин
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 - 10.18287/1998-6629-2014-0-5-1(47)-124-131
Subject(s) - injector , thrust , nozzle , combustion chamber , fuel injection , rocket engine , rocket (weapon) , materials science , aerospace engineering , mechanics , combustion , mechanical engineering , liquid fuel , engineering , nuclear engineering , automotive engineering , physics , chemistry , organic chemistry