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
   
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
   
Thrust: 44,000 kgf (sl)
Burn time: 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 (v)
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 (v)
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


 
  
S1.35800
   
Propellant: O2 / Kerosene
Thrust: 2,865 kgf (sl)
 
 
  
RD-0109
   
Propellant: O2 / Kerosene
Thrust: 5,559 kgf (v)
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 (v)
Burn time: 250 s
Specific impulse: 326 s (v)
Launch vehicles: Molniya,
Voskhod, Soyuz

First flight: 1960


 
  
RD-0124
   
Thrust: 30,010 kgf
Burn time: 300 s (v)
Specific impulse: 359  s (v)
Launch vehicles: Soyuz, Angara
First flight: 2006
 
 
  
RD-0154
   
Propellant: O2 / Kerosene
Thrust: 30,010 kgf
Specific impulse: 363 s (v)
 
 
  
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
   
Propellant: N2O4 / (CH3)2NNH2
Thrust (sl): 178,246 kgf (v)
Thrust (sl): 160,605 kgf (sl)
Specific impulse: 315 s (v)
Specific impulse: 284 s (sl)
Launch vehicles: Proton
First flight: 1965


  
RD-275
   
Propellant: N2O4 / (CH3)2NNH2
Thrust (sl): 178,144 kgf (v)
Thrust (sl): 162,236 kgf (sl)
Specific impulse: 315 s (v)
Specific impulse: 278 s (sl)
Launch vehicles: Proton
First flight: 1986


  
RD-275M
   
Propellant: N2O4 / (CH3)2NNH2
Thrust (sl): 186,302 kgf (v)
Thrust (sl): 170,394 kgf (sl)
Burn time:  130 s
Specific impulse: 322 s (v)
Specific impulse: 294 s (sl)
Launch vehicles: Proton
 
 
  
RD-0202 (RD-0203 / 0204)
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 50,883 kgf (sl)
Thrust: 56,900 kgf (v)
Burn time:  136 s
Specific impulse: 311 s (v)
Specific impulse: 278 s (sl)
Launch vehicles: UR-200
First flight: 1964
 
  
RD-0205
(1 x RD-0206 + 4 x RD-0207)
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 61,835 kgf (v)
Burn time: 150 s
Specific impulse: 322 s (v)
Launch vehicles: UR-200
First flight: 1967


  
RD-0207
Thrust: 775 kgf (v)
 
 
  
RD-0208 / 0209
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 58,500 kgf (v)
Specific impulse: 327 s (v)
Launch vehicles: UR-500, Proton
First flight: 1965
 
 
  
RD-0210 / 0211
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 59,357 kgf (v)
Burn time:  230 s
Specific impulse: 327 s (v)
Launch vehicles: Proton
First flight: 1967


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


  
RD-0214
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 787 kgf (v)
 
 
  
RD-0216
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 22,127 kgf (v)
Thrust: 19,986 kgf (sl)
Specific impulse: 279 s (v)
Specific impulse: 312 s (sl)
Launch vehicles: UR-100
First flight: 1965
 
 
  
RD-0233
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 52,617 kgf (v)
Thrust: 47,722 kgf (sl)
Burn time: 121 s
Specific impulse: 285 s (v)
Specific impulse: 310 s (sl)
Launch vehicles:UR-100N(U), Strela, Rockot
First flight: 1972
 
 
  
RD-268
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 125,425 kgf (v)
Thrust: 116.859 kgf (sl)
Burn time: 121 s
Specific impulse: 296 s (v)
Specific impulse: 319 s (sl)
Launch vehicles:MR-UR-100(U)
First flight: 1971
 
 
  
RD-264 (4x RD-263)
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 461,115 kgf (v)
Thrust: 424,813 kgf (sl)
Specific impulse: 293 s (v)
Specific impulse: 318 s (sl)
Launch vehicles:R-36M(U)
First flight: 1977
 
 
  
RD-0228
   
(1 x RD-0229 + 4 x RD-0230)
Propellant: N2O4 / (CH3)2NNH2
Thrust:  77,498 kgf (v)
Specific impulse:340 s (v)
Launch vehicles: R-36M(U)
First flight: 1971
RD-0230


 
  
RD-0255
   
(1 x RD-0256 + 4 x RD-0257)
Propellant: N2O4 / (CH3)2NNH2
Thrust:  85,248 kgf (v)
Specific impulse:340 s (v)
Launch vehicles: R-36M2
First flight: 1986
RD-0257
 
 
  
RD-0243
   
(1 x RD-0244 + 4 x RD-0245
Propellant: N2O4 / (CH3)2NNH2
Thrust: 69,544 kgf (v)
Thrust: 63,018 kgf (sl)
Burn time: 79 s
Specific impulse: 288 s (v)
Specific impulse: 321 s (sl)
Launch vehicles: R-29, R-29R(M), Volna, Shtil
First flight: 1977
RD-0245
Thrust: 19,170 kgf (v)
Thrust: 21,719 kgf (sl)
Burn time: 79 s
Specific impulse: 254 s (v)
Specific impulse: 288 s (sl)
 
 
  
RD-0235
   
Propellant: N2O4 / (CH3)2NNH2
Thrust:  24,473 kgf (v)
Specific impulse:320 s (v)
Launch vehicles: UR-100N(U), Strela, Rockot
First flight: 1972
RD-0236
   
Thrust: 1,607 kgf (v)
 
  
RD-862
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 14,544 kgf (v)
Burn time: 195 s
Specific impulse: 331 s
Launch vehicles: MR-UR-100(U)
First flight: 1971
 
 
  
NK-9
   
Propellant: O2 / Kerosene
Thrust: 45,000 kgf (v)
Thrust: 36,750 kgf (sl)
Specific impulse: 328 s (v)
Specific impulse: 286 s (sl)
Launch vehicles: GR-1
 
 
  
NK-9v
   
Propellant: O2 / Kerosene
Thrust: 45,000 kgf (v)
Specific impulse: 345 s (v)
Launch vehicles: GR-1
unflown


 
  
NK-19
   
Propellant: O2 / Kerosene
Thrust: 46,000 kgf (v)
Specific impulse: 345 s (v)
Launch vehicles: N1
First flight: 1969
 
 
  
NK-21
   
Propellant: O2 / Kerosene
Thrust: 40,992 kgf (v)
Specific impulse: 340 s (v)
Launch vehicles: N1
First flight: 1969


 
  
NK-39
   
Propellant: O2 / Kerosene
Thrust: 41,706 kgf (v)
Specific impulse: 352 s (v)
Launch vehicles: N1F (unflown)
 
 
  
NK-15
   
Propellant: O2 / Kerosene
Thrust: 157,444 kgf (v)
Thrust: 154,000 kgf (sl)
Burn time: 113 s
Specific impulse: 318 s (v)
Specific impulse: 297 s (sl)
Launch vehicles: N1
First flight: 1969
 
 
  
NK-15v
   
Propellant: O2 / Kerosene
Thrust: 168,000 kgf (v)
Specific impulse: 325 s (v)
Launch vehicles: N1
First flight: 1969
 
 
  
NK-33
   
Propellant: O2 / Kerosene
Thrust: 167,000 kgf (v)
Thrust: 154,181 kgf (sl)
Burn time: 600 s
Specific impulse: 331 s (v)
Specific impulse: 297 s (sl)
Launch vehicles: N1F
First flight: unflown
 
  
NK-33
   
Propellant: O2 / Kerosene
Thrust: 167,000 kgf (v)
Thrust: 154,181 kgf (sl)
Burn time: 600 s
Specific impulse: 334 s (v)
Specific impulse: 300 s (sl)
Launch vehicles: Soyuz-2.1v
First flight: 2013
 
  
NK-33 (AJ26-62)
   
Propellant: O2 / Kerosene
Thrust: 167,000 kgf (v)
Thrust: 154,181 kgf (sl)
Burn time: 600 s
Specific impulse: 334 s (v)
Specific impulse: 300 s (sl)
Launch vehicles: Antares 1
First flight: 2013
 
 
  
NK-43
   
Propellant: O2 / Kerosene
Thrust: 181,000 kgf (v)
Thrust: 127,237 kgf (sl)
Burn time: 600 s
Specific impulse: 346 s (v)
Specific impulse: 246 s (sl)
First flight: unflown


  
NK-43 (AJ26-60)
   
Launch vehicles: Kistler K-1
 
 
 
  
RD-170 / 170M
   
Propellant: O2 / Kerosene
Thrust: 806.76 kgf (v)
Thrust: 769,876 kgf (sl)
Burn time: 150 s
Specific impulse: 337 s (v)
Specific impulse: 309 s (sl)
Launch vehicles: Energia
First flight: 1985


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


 
  
RD-172
   
Propellant: O2 / Kerosene
Thrust (sl): 783,998 kgf (sl)
Specific impulse: 337 s (v)
Specific impulse: 310 s (sl)
Launch vehicles: Vulkan
First flight: unflown
 
  
RD-180 
   
Propellant: O2 / Kerosene
Thrust (sl): 423.386 kgf (sl)
Burn time: 270 s
Specific impulse: 339 s (v)
Specific impulse: 313 s (sl)
Launch vehicles: Atlas 3 / 5
First flight: 2000
 
 
  
RD-190
   
Propellant: O2 / Kerosene


 
  
RD-191
   
Propellant: O2 / Kerosene
Thrust (sl): 212,000 kgf (sl)
Burn time: 270 s
Specific impulse: 337 s (v)
Specific impulse: 311 s (sl)
Launch vehicles: Angara, KSLV
First flight: 2009
 
 
  
RD-193
   
Propellant: O2 / Kerosene
Thrust (sl): 212,000 kgf (sl)
Burn time: 270 s
Specific impulse: 337 s (v)
Specific impulse: 311 s (sl)
Launch vehicles: Soyuz
First flight: unflown
 
 
  
RD-181
   
Propellant: O2 / Kerosene
Thrust (sl): 185,894 kgf (sl)
Burn time: 270 s
Specific impulse: 338 s (v)
Specific impulse: 312 s (sl)
Launch vehicles: Antares 2
First flight: 2013
 
 
  
RD-120
   
Propellant: O2 / Kerosene
Thrust: 85,003 kgf (v)
Burn time: 315  s
Specific impulse: 350 s (v)
Launch vehicles: Zenit 2
  
First flight: 1985


 
  
RD-120
   
Propellant: O2 / Kerosene
Thrust: 92,998 kgf (v)
Specific impulse: 350 s (v)
Launch vehicles: Zenit 3SL
  
First flight: 1999
 
 
  
RD-120U
   
Propellant: O2 / Kerosene
Thrust: 88,786 kgf (v)
Thrust: 77,855 kgf (sl)
Burn time: 315  s
Specific impulse: 294 s (v)
Specific impulse: 294 s (sl)


 
  
RD-120M
   
Propellant: O2 / Kerosene
Thrust: 89,408 kgf (v)
Thrust: 79,303 kgf (sl)
Burn time: 315  s
Specific impulse: 340 s (v)
Specific impulse: 301 s (sl)
Launch vehicles: Soyuz-M
 
 
  
RD-182
   
Propellant: O2 / CH4
Thrust: 90,856 kgf (v)
Thrust: 79,303 kgf (sl)
Specific impulse: 353 s (v)
Specific impulse: 316 s (sl)
 
 
  
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
 
  
RD-810
   

 
  
SCE-200
   
Propellant: O2 / Kerosene
Thrust (sl): 214,548 kgf (v)
Thrust (sl): 191,298 kgf (sl)
Specific impulse: 335 s (v)
Specific impulse: 299 s (sl)
Launch vehicles: ULV (LMV3)
 
  
YF-100K
   
Propellant: O2 / Kerosene
Thrust (sl): 125,527 kgf (v)
Thrust (sl): 140,312 kgf(sl)
Specific impulse: 337 s (v)
Specific impulse: 302 s (sl)
Launch vehicles: CZ-5

 
 
  
RD-58
   
Propellant: O2 / Kerosene
Thrust: 8.504 kgf (v)
Burn time: 600 s
Specific impulse: 349 s (v)
Launch vehicles: Proton, N1
First flight: 1967
 
 
  
RD-58 S
   
Propellant: O2 / Sintin
Thrust: 8,763 kgf (v)
Burn time: 680 s
Specific impulse: 361 s (v)
Launch vehicles: Proton

 
 
  
RD-58 M
   
Propellant: O2 / Kerosene
Thrust: 8,668 kgf (v)
Burn time: 600 s
Burn time: 775 s
Specific impulse: 356 s (v)
Launch vehicles: Proton
First flight: 1974
 
 
  
(17D12)
   
Thrust: 8,800 kgf (v)
Burn time: 680 s
Specific impulse: 362 s (v)
Launch vehicles: Buran OMS,
 
 
  
RD-58 Z  (carbon nozzle)
Propellant: O2 / Kerosene
Thrust: 8,102 kgf (v)
Burn time: 640 s
Burn time: 695 s
Specific impulse: 361 s (v)
Launch vehicles: Zenit
 
 
  
RD-58 MFD
   

 
 
  
RD-58 MF
   
Propellant: O2 / Kerosene
Thrust: 5,007 kgf (v)
Burn time: 1,400 s
Specific impulse: 372 s (v)
 
 
  
RD-56 (KVD-1)
   
Propellant: O2 / H2
Thrust (sl): 7,097 kgf (v)
Burn time: 800 s
Specific impulse: 462 s (v)


 
  
RD-56 (KVD-1)
   
Propellant: O2 / H2
Thrust (sl): 7,097 kgf (v)
Specific impulse: 462 s (v)
Launch vehicles: GSLV Mk1
First flight: 1993
 
 
  
RD-0146
   
Propellant: O2 / H2
Thrust (sl): 10,003 kgf (v)
Burn time: 1100 s
Specific impulse: 462 s (v)


 
  
RD-0146D
   
Propellant: O2 / H2
Thrust (sl): 7,494 kgf (v)
Specific impulse: 470 s (v)


 
  
RD-0146E
   
Propellant: O2 / H2
Thrust (sl): 10,003 kgf (v)
Specific impulse: 470 s (v)
 
  
RD-0120
   
Propellant: O2 / H2
Thrust: 199,966 kgf (v)
Thrust: 147,960 kgf (sl)
Burn time: 600 s
Specific impulse: 455 s (v)
Specific impulse: 359 s (sl)
Launch vehicles: Energia
First flight: 1987

 
 
  
RD-0126
   
Propellant: O2 / H2
Thrust (sl): 3,997 kgf (v)
Specific impulse: 470 s (v)
 
 
  
RD-0126E
   
Propellant: O2 / H2
Thrust (sl): 3,997 kgf (v)
Specific impulse: 472 s (v)
 
 
  
RD-161
   
Propellant: O2 / Kerosene
Thrust: 2,000 kgf (v)
Burn time: 900 s
Specific impulse: 360 s (v)
 
 
  
RD-161
   
Propellant: O2 / Kerosene
Thrust: 2,030 kgf (v)
Burn time: 900 s
Specific impulse: 365 s (v)
 
 
 
  
RD-119
   
Propellant: O2 / (CH3)2NNH2
Thrust: 10,758 kgf (v)
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 (v)
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 (v)
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 (v)
Burn time: 130 s
Specific impulse: 317 s
Launch vehicles: Tsiklon-2 / 3
First flight: 1965
 
 
  
s1.5400 (8D726)
   
Propellant: O2 / Kerosene
Thrust: 6,801 kgf (v)
Burn time: 208 s
Launch vehicles: Molniya
First flight: 1965
 
 
  
S 5.4612
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 299 kgf (v)
Specific impulse: 307 s (v)
Launch vehicles: Soyuz-Ikar
 
 
  
S 5.92
   
Propellant: N2O4 / (CH3)2NNH2
Thrust: 2,000 kgf (v)
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 (v)
Burn time: 3,200 s
Specific impulse: 326 s (v)
Launch vehicles: Rokot, Proton-Briz M, Angara-Briz M
First flight: 1990