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bn:12537056n
Noun Concept
ES
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
propulsor Vernier
PART OF
Protón
Rokot
SOURCE OF ENERGY
1,1-dimetilhidrazina
tetróxido de dinitrógeno

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