RD-100
  
Propellant: O2 / Alcohol
Thrust: 27,227 kgf (sl)
Burn time: 65 s
Specific impulse: 237 s (v)
Specific impulse: 203 s (sl)
Launch vehicles: R-1
First flight: 1948

  
RD-101
  
Propellant: O2 / Alcohol
Thrust: 37,19 (sl)
Burn time: 83 s
Specific impulse: 235 s (v)
Specific impulse: 214 s (sl)
Launch vehicles: R-2
First flight: 1951

  
RD-103
  
Propellant: O2 / Alcohol
Thrust: 44,000 kgf (sl)
Burn time: 83 / 120 s
Specific impulse: 243 s (v)
Specific impulse: 216 s (sl)
Launch vehicles: R-5
First flight: 1953
 

 
 

  
S 2.253
  
Propellant: HNO3 / Kerosene
Thrust: 9,513 kgf (v)
Thrust: 8,300 kgf (sl)
Specific impulse: 95 s (v)
Specific impulse: 219 s (sl)
Launch vehicles: R-11
First flight: 1953


  
S 5.2
  
Propellant: HNO3 / Kerosene
Thrust: 13,378 kgf (v)
Thrust: 13,380 kgf (sl)
Specific impulse: 258 s (v)
Specific impulse: 226 s (sl)
Launch vehicles: R-17
First flight: 1961
 

 
 

  
RD-107
  
Propellant: O2 / Kerosene
Thrust: 99,014 kgf
Thrust: 80,884 kgf (sl)
Burn time: 140 s
Specific impulse: 306 s (v)
Specific impulse: 250 s (sl)


  
RD-108
  
Propellant: O2 / Kerosene
Thrust: 92,998 kgf
Thrust: 72,768 kgf (sl)
Burn time: 340 s
Specific impulse: 308 s (v)
Specific impulse: 241 s (sl)
Launch vehicles: R-7, Vostok, Voskhod, Molniya, Soyuz
First flight: 1957
 

 
 

  
RD-0109
  
Propellant: O2 / Kerosene
Thrust: 5,559 kgf
Burn time: 430 s
Specific impulse: 324 s (v)
Launch vehicles: Vostok
First flight: 1960
 

 
 

  
RD-0106
  
Launch vehicles: R-9


  
RD-0107 / 0108 / 0110
  
Propellant: O2 / Kerosene
Thrust: 30,377 kgf
Burn time: 250 s
Specific impulse: 326 s
Launch vehicles: Molniya,
Voskhod, Soyuz

First flight: 1960

 

  
RD-0124
  
Thrust: 30,010 kgf
Burn time: 300 s
Specific impulse: 359  s
Launch vehicles: Soyuz, Angara
First flight: 2006
 

 
 

  
RD-214
  
Propellant: HNO3 / Kerosene
Thrust: 74,439 kgf (v)
Thrust: 64,752 kgf (sl)
Burn time: 140 s
Specific impulse: 264 s (v)
Specific impulse: 230 s (sl)
Launch vehicles: R-12, Kosmos
First flight: 1957
 

 
 

  
RD-216
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 176,207 kgf (v)
Thrust: 149,796 kgf (sl)
Burn time: 146 s
Specific impulse: 291 s (v)
Specific impulse: 248 s (sl)
Launch vehicles: R-14, Kosmos, Kosmos 3 / 3M
First flight: 1964
 

 
 

  
  
RD-218 (3 x RD-217)
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 264,310 kgf (v)
Thrust: 226,400 kgf kgf (sl)
Burn time: 90 s
Specific impulse: 289 s (v)
Specific impulse: 246 s (sl)
Launch vehicles: R-16
First flight: 1960


  
RD-251 (3 x RD-250)
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 269,510 kgf (v)
Thrust: 241,264 kgf (sl)
Burn time: 120 s
Specific impulse: 301 s (v)
Specific impulse: 269 s (sl)
Launch vehicles: R-36, Tsiklon
First flight: 1965
 

 
 

  
RD-219
  
Propellant: HNO3 / (CH3)2NNH2
Thrust: 90,040 kgf (v)
Burn time: 125 s
Specific impulse: 293 s (v)
Launch vehicles: R-16
First flight: 1960
 

 
 

  
RD-252
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 95,904 kgf (v)
Burn time: 160 s
Specific impulse: 317 s (v)
Launch vehicles: R-36, Tsiklon
First flight: 1965


  
RD-253 / 275
  
Propellant: N2O4 / (CH3)2NNH2
Thrust (sl): 177,940 kgf
Burn time: 130 s
Specific impulse: 317 s (v)
Specific impulse: 285 s (sl)
Launch vehicles: Proton
First flight: 1965

 

 
 

  
RD-0202 (RD-0203 / 0204)
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 57,002 kgf
Burn time:  136 s
Specific impulse: 311 s
Launch vehicles: UR-200
First flight: 1964


  
RD-0208 / 0209
  
Launch vehicles: UR-500, Proton
First flight: 1965


  
RD-0205
(1 x RD-0206 + 4 x RD-0207
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 61,835 kgf
Burn time: 150 s
Specific impulse: 322 s
Launch vehicles: UR-200
First flight: 1967
 

 
 

  
RD-0210 / 0211
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 59,357 kgf
Burn time:  230 s
Specific impulse: 327 s
Launch vehicles: Proton
First flight: 1967



  
RD-0212
(1 x RD-0213 + 4 x RD-0214)
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 62,508 kgf
Burn time:  230 s
Specific impulse: 325 s
Launch vehicles: Proton
First flight: 1967

 

 
 

  
RD-170 / 171
  
Propellant: O2 / Kerosene
Thrust (sl): 769,876 kgf
Burn time: 150 s
Specific impulse: 337 s (v)
Specific impulse: 309 s (sl)
Launch vehicles: Energia, Vulkan, Energia M, Zenit
First flight: 1985
 

 
 
 

  
RD-180
  
Propellant: O2 / Kerosene
Thrust (sl): 423.386 kgf
Burn time: 270 s
Specific impulse: 339 s (v)
Specific impulse: 313 s (sl)
Launch vehicles: Atlas 3 / 5
First flight: 2000
 

 
 

  
RD-191 / 181
  
Propellant: O2 / Kerosene
Thrust (sl): 212,000 kgf
Burn time: 270 s
Specific impulse: 337 s (v)
Specific impulse: 311 s (sl)
Launch vehicles: Angara, KSLV, Antares 2
First flight: 2009


  
RD-0120
  
Propellant: O2 / H2
Thrust (sl): 199,966 kgf
Burn time: 600 s
Specific impulse: 455 s (v)
Specific impulse: 359 s (sl)
Launch vehicles: Energia
First flight: 1987

 

 
 

  
NK-15
  
Propellant: O2 / Kerosene
Thrust: 157,444 kgf
Thrust: 154,000 kgf (sl)
Burn time: 113 s
Specific impulse: 318 s (v)
Specific impulse: 297 s (sl)


  
  
NK-15v
  
Thrust: 168,000 kgf
Specific impulse: 325 s (v)


  
  
NK-19 / NK-21 / NK-9v
  
Thrust: 45,000 kgf
Specific impulse: 312 s (v)
Launch vehicles: N1
First flight: 1969
 

 
 

  
NK-33
  
Propellant: O2 / Kerosene
Thrust: 167,000 kgf
Thrust: 154,000 kgf (sl)
Burn time: s
Specific impulse: 331 s (v)
Specific impulse: 297 s (sl)
Launch vehicles: N1


  
NK-43
  
Propellant: O2 / Kerosene
Thrust: 181,000 kgf
Thrust: 127,237 kgf (sl)
Burn time: 600 s
Specific impulse: 346 s (v)
Specific impulse: 246 s (sl)
Launch vehicles: N1

 

  
NK-33
  
Launch vehicles: Soyuz-2.1v
First flight: 2013


  
NK-33 (AJ26-62)
Launch vehicles: Antares 1
First flight: 2013


  
NK-43 (AJ26-60)
Launch vehicles: Kistler K-1
 

 
 

  
RD-120
  
Propellant: O2 / Kerosene
Thrust (sl): 84,942 kgf
Burn time: 315  s
Specific impulse: 350 s (v)
Launch vehicles: Zenit
  
First flight: 1985
 

 
 

  
RD-58 / 58 M
  
Propellant: O2 / Kerosene
Thrust: 8.504 kgf
Burn time: 680 s
Specific impulse: 353 s (v)
Launch vehicles: N1, Proton, Angara, Buran OMS,
First flight: 1967
 

 
 

  
s1.5400
  
Propellant: O2 / Kerosene
Thrust: 6,801 kgf
Burn time: 208 s
Launch vehicles: Molniya
First flight: 1965
 

 
 

  
RD-119
  
Propellant: O2 / (CH3)2NNH2
Thrust: 10,758 kgf
Burn time: 260  s
Specific impulse: 352 s (v)
Launch vehicles: Kosmos
First flight: 1961
 

 
 

  
S 5.23 (11D49)
  
Propellant: HNO3 / (CH3)2NNH2
Thrust: 16,060 kgf
Burn time: 4,305 s
Specific impulse: 303 s (v)
Launch vehicles: Kosmos-3M
First flight: 1964


  
RD-854
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 7,698 kgf
Burn time: 70 s
Specific impulse: 312 s
Launch vehicles: R-36orb
First flight: 1962


  
RD-861
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 8,026 kgf
Burn time: 130 s
Specific impulse: 317 s
Launch vehicles: Tsiklon-2 / 3
First flight: 1965


  
RD-862
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 14,544 kgf
Burn time: 195 s
Specific impulse: 331 s
Launch vehicles: MR-UR-100
First flight: 1971
 

 
 

  
S 5.92
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 2,000 kgf
Burn time: 2,000 s
Specific impulse: 327 s (v)
Launch vehicles: Soyuz-Fregat
First flight: 2000
 

 
 

  
S 5.98M
  
Propellant: N2O4 / (CH3)2NNH2
Thrust: 2,000 kgf
Burn time: 3,200 s
Specific impulse: 326 s (v)
Launch vehicles: Rokot, Proton-Briz M, Angara-Briz M
First flight: 1990