e/YF-75

Information
has gloss	eng: YF-75 (Rocket Engine) The YF-75 is China's second generation of cryogenic gimballed engine, using liquid hydrogen (LH2) fuel and liquid oxygen (LOX) oxidizer. Its development began in the early 1990s and its first flight was in 1994. Specifications Vacuum thrust: 78.45 kN Vacuum specific impulse: 437 s Burn time: 470 s Engine weight: 550 kg Exit to Throat Area ratio: 80 to 1 Propellants: LOX & LH2 *Mixture ratio: 5.00
lexicalization	eng: YF-75
instance of	(noun) a jet engine containing its own propellant and driven by reaction propulsion rocket engine, rocket