YF-50
Propellant: N2O4 / (CH3)NHNH2
Thrust: 49 kgf (v)
Specific impulse: ? (v)
Launch vehicles: Satellites,
Space Tugs
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YF-50D
Propellant: N2O4 / (CH3)2NNH2
Thrust: 255 kgf (sl)
Specific impulse: 219 s (v)
Launch vehicles: Shenzou, Tiangong, Tianzhou, CMS
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