Login Preferences
About News Publications Statistics Downloads API Guide License How to use Preferences
bn:12537056n
Noun Concept
FR
No term available
EN
Isayev N2O4/UDMH rocket engine. 0.392 kN. In Production. Isp=252s. Small attitude control thruster in Briz upper stage Wikidata
Relations
Sources
IS A
moteur vernier
PART OF
Proton
Rokot
SOURCE OF ENERGY
1,1-diméthylhydrazine
peroxyde d'azote

Please note that, in order to improve your browsing experience on this website, BabelNet® uses various types of cookies, including: browsing functionality, performance and statistical cookies.

By continuing to browse the site you are agreeing to our use of cookies. OK

License