YF-2
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 31,213 kgf (sl)
Burn time: 130 s
Specific impulse: 241 s (v)
Specific impulse: 268 s (sl)
Launch vehicles: CZ 1
First flight: 1969
 
 
  
YF-20
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 76,499 kgf (sl)
Burn time: 132 s
Specific impulse: 289 s (v)
Specific impulse: 259 s (sl)
Launch vehicles: FB-1, CZ 2A
First flight: 1972
  
YF-21 (4 x YF-20)
YF-21A (4 x YF-20A)
YF-21A (4 x YF-20A)
YF-21A (4 x YF-20A)
 
 
  
YF-20A
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 76,499 kgf (sl)
Burn time: 132 s
Specific impulse: 289 s (v)
Specific impulse: 259 s (sl)
Launch vehicles: CZ 2C / 3
First flight: 1982
 
 
  
YF-20B
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 83,239 kgf (sl)
Burn time: 170 s
Specific impulse: 289 s (v)
Specific impulse: 259 s (sl)
Launch vehicles: CZ 2D / 2E /
2F / 3A / 4 / 4B

First flight: 1988
 
 
  
YF-20C / F-25
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 80,292 kgf (sl)
Specific impulse: 297 s (v)
Specific impulse: 260 s (sl)
Launch vehicles: CZ 3B / 3C / 4C
First flight: 1999
 
 
  
YF-22
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 73,195kgf (sl)
Specific impulse: 295  s (v)
Specific impulse: 260 s (sl)
Launch vehicles: CZ 3B / 3C / 4C
First flight: 1999
  
YF-22A / 22B
 
 
  
YF-24 (YF-22 + 4 x YF-23)
YF-24A (YF-22A + 4 x YF-23)
YF-24B (YF-22B + 4 x YF-23)
 
 
  
YF-22E
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 80,292 kgf (sl)
Burn time: 170 s
Specific impulse: 297 s (v)
Specific impulse: 260 s (sl)
Launch vehicles: CZ 3B / 3C / 4C
First flight: 1999
 
 
  
YF-24D (YF-22E + 4 x YF-23B)
YF-24E (YF-22BE + 4 x YF-23)F
 
 
  
YF-40
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 10,003 kgf (v)
Specific impulse: 303 s (v)
Specific impulse: 297 s (sl)
Launch vehicles: CZ 4
First flight: 1999
 
 
  
YF-50
   
Propellant: N2O4 / (CH3)NHNH2
Thrust: 49 kgf (v)
Specific impulse: ? (v)
Launch vehicles: Satellites,
Space Tugs

 
 
  
YF-50D
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 255 kgf (sl)
Specific impulse: 219 s (v)
Launch vehicles: Shenzou, Tiangong, Tianzhou, CMS
 
 
  
YF-100
   
Propellant: O2 / Kerosene
Thrust (sl): 124,762 kgf (v)
Thrust (sl): 139,395 kgf (sl)
Specific impulse: 335 s (v)
Specific impulse: 300 s (sl)
Launch vehicles: CZ-5 / 6 / 7
First flight: 2016


 
  
YF-100GBI
Launch vehicles: CZ-6
First flight: 2015


 
  
YF-100F
 
 
  
YF-100K
   
Propellant: O2 / Kerosene
Thrust (sl): 140,312 kgf (v)
Thrust (sl): 125,527 kgf (sl)
Specific impulse: 337 s (v)
Specific impulse: 302 s (sl)
Launch vehicles: CZ-5



 
 
  
YF-115
   
Propellant: O2 / Kerosene
Thrust (sl): 17,997 kgf (v)
Burn time: 341 s
Specific impulse: 342 s (v)
Specific impulse: 294 s (sl)
Launch vehicles: CZ-6 / 7
First flight: 2015
 
 
  
YF-73
   
Propellant: O2 / H2
Thrust: 4,502 (v)
Specific impulse: 420 (v)
Launch vehicles: CZ-3
First flight: 1984
  
 
 
  
YF-75
   
Propellant: O2 / H2
Thrust: 15,999 (v)
Specific impulse: 437 (v)
Launch vehicles: CZ-3A / B / C
First flight: 1994
  
 
 
  
YF-77
   
Propellant: O2 / H2
Thrust: 52,821 (v)
Thrust: 71,380 (sl)
Specific impulse: 428 (v)
Specific impulse: 312 (sl)
Launch vehicles: CZ-5
First flight: 2016