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