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50 n thrust correction engine for the "Luna-resurs" lunar module descent engine
Author(s) -
Ю. И. Агеенко,
И. В. Пегин,
Д. В. Чесноков
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)-112-117
Subject(s) - rocket engine , combustion chamber , propellant , nozzle , rocket engine nozzle , materials science , thrust , mechanical engineering , conical surface , chamber pressure , liquid propellant rocket , combustion , aerospace engineering , mechanics , nuclear engineering , composite material , chemistry , engineering , metallurgy , physics , organic chemistry

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