RD-100 Propellant: Thrust: 27,227 kgf (sl) Chamber pressure: 16 atm Burn time: 65 s Specific impulse: 237 s (v) Specific impulse: 203 s (sl) Vehicles: R-1 First flight: 1948

RD-101     Propellant: Chamber pressure: 21 atm Thrust: 37,19 (sl) Burn time: 83 s Specific impulse: 235 s (v) Specific impulse: 214 s (sl) Vehicles: R-2 First flight: 1951

RD-103     Propellant: Chamber pressure: 23 atm Thrust: 44,000 kgf (sl) Burn time: 120 s Specific impulse: 243 s (v) Specific impulse: 216 s (sl) Vehicles: R-5 First flight: 1953

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

S 5.2     Propellant: Chamber pressure: 67 atm Thrust: 13,378 kgf (v) Thrust: 13,380 kgf (sl) Specific impulse: 258 s (v) Specific impulse: 226 s (sl) Vehicles: R-17 First flight: 1961

RD-107 / RD-108     Propellant: Chamber pressure: 56 / 48 atm Thrust: 99,014 / 92,998 kgf (v) Thrust: 80,884 / 72,768 kgf (sl) Burn time: 140 / 340 s Specific impulse: 306 / 308 s (v) Specific impulse: 250 / 241 s (sl) Vehicles: R-7, Vostok, Voskhod, Molniya, Soyuz (1 / 2 st.) First flight: 1957    S1.35800     Propellant: Thrust: 2,865 kgf (sl)    RD-107MM / RD-108MM     Propellant: Chamber pressure: 58 / 52 atm Thrust: 101,971 / 99,055 kgf (v) Thrust: 83,524 / 79,313 kgf (sl) Specific impulse: 314 / 316 s (v) Specific impulse: 257 / 253 s (sl) Vehicles: Molnya-M  (1 / 2 st.) First flight: 1965    RD-117 / RD-118     Propellant: Chamber pressure: 58 / 52 atm Thrust: 101,971 / 99,055 kgf (v) Thrust: 83.524 / 79,313 kgf (sl) Specific impulse: 314 / 316 s (v) Specific impulse: 257 / 253 s (sl) Vehicles: Soyuz-U  (1 / 2 st.) First flight: 1973    RD-117P / RD-118P     Propellant: Vehicles: Soyuz-U2  (1 / 2 st.) First flight: 1982    RD-107A / RD-108A     Propellant: Chamber pressure: 59 / 54 atm Thrust: 104,051 / 100,503 kgf (v) Thrust: 85,5648 / 80,802 kgf (sl) Specific impulse: 320 / 320 s (v) Specific impulse: 263 / 257 s (sl) Vehicles: Soyuz-FG / -2  (1 / 2 st.) First flight: 2001

RD-111     Propellant: Chamber pressure: 77 atm Thrust: 166,009 kgf (sl) Thrust: 144,085 kgf (v) Burn time: 110 s Specific impulse: 317 s (v) Specific impulse: 275 s (sl) Vehicles: R-9  (1 st.) First flight: 1961

RD-0109     Propellant: Chamber pressure: 49 atm Thrust: 5,559 kgf (v) Burn time: 430 s Specific impulse: 324 s (v) Vehicles: Vostok (3 st.) First flight: 1960

RD-0106     Propellant: Burn time: 140 s Vehicles: R-9 (2 st.) First flight: 1961

RD-0107 / 0108     Propellant: Chamber pressure: 67 atm Thrust: 30,622 kgf (v) Burn time: 250 s Specific impulse: 330 s (v) Vehicles: Molniya / Voskhod (3 st.) First flight: 1960

RD-0110     Propellant: Chamber pressure: 153 atm Thrust: 30,377 / 30,754 kgf (v) Burn time: 250 s Specific impulse: 326 / 330 s (v) Vehicles: Molniya M, Soyuz (3 st.) First flight: 1965

RD-0124     Propellant: Chamber pressure: 155 atm Thrust: 30,010 kgf (v) Burn time: 300 s (v) Specific impulse: 359  s (v) Vehicles: Soyuz (3 st.), Vehicles: Angara (3 or 2 st.) First flight: 2006

RD-0154     Propellant: Chamber pressure: 150 atm Thrust: 30,010 kgf Specific impulse: 363 s (v) Vehicles: Aurora (3 st.) First flight: unflown

RD-214     Propellant: Chamber pressure: 43 atm Thrust: 74,439 kgf (v) Thrust: 64,752 kgf (sl) Burn time: 140 s Specific impulse: 264 s (v) Specific impulse: 230 s (sl) Vehicles: R-12, Kosmos  (1 st.) First flight: 1957

RD-216     Propellant: Chamber pressure: 73 atm Thrust: 176,207 kgf (v) Thrust: 149,796 kgf (sl) Burn time: 146 s Specific impulse: 291 s (v) Specific impulse: 248 s (sl) Vehicles: R-14 Vehicles: Kosmos / 3 / 3M  (1 st.) First flight: 1964

RD-218 (3 x RD-217     Propellant: Chamber pressure: 73 atm 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) Vehicles: R-16  (1 st.) First flight: 1960    RD-251 (3 x RD-250)     Propellant: Chamber pressure: 82 atm Thrust: 269,510 kgf (v) Thrust: 241,264 kgf (sl) Burn time: 120 s Specific impulse: 301 s (v) Specific impulse: 269 s (sl) Vehicles: R-36, Tsiklon  (1 st.) First flight: 1965

RD-219     Propellant: Chamber pressure: 73 atm Thrust: 90,040 kgf (v) Burn time: 125 s Specific impulse: 293 s (v) Vehicles: R-16 (2 st.) First flight: 1960

RD-252     Propellant: Chamber pressure: 88 atm Thrust: 95,904 kgf (v) Burn time: 160 s Specific impulse: 317 s (v) Vehicles: R-36, Tsiklon (2 st.) First flight: 1965

RD-253     Propellant: Chamber pressure: 145 atm Thrust: 178,246 kgf (v) Thrust: 160,605 kgf (sl) Specific impulse: 315 s (v) Specific impulse: 284 s (sl) Vehicles: Proton  (1 st.) First flight: 1965    RD-275     Propellant: Chamber pressure: 155 atm Thrust: 178,144 kgf (v) Thrust: 162,236 kgf (sl) Specific impulse: 315 s (v) Specific impulse: 278 s (sl) Vehicles: Proton  (1 st.) First flight: 1986    RD-275M     Propellant: Chamber pressure: 164 atm Thrust: 186,302 kgf (v) Thrust: 170,394 kgf (sl) Burn time:  130 s Specific impulse: 322 s (v) Specific impulse: 294 s (sl) Vehicles: Proton  (1 st.)

RD-0202 (RD-0203 / 0204)     Propellant: Thrust: 50,883 kgf (sl) Thrust: 56,900 kgf (v) Burn time:  136 s Specific impulse: 311 s (v) Specific impulse: 278 s (sl) Vehicles: UR-200  (1 st.) First flight: 1964

RD-0205 (1 x RD-0206 + 4 x RD-0207)     Propellant: Chamber pressure: 145 atm Thrust: 61,835 kgf (v) Burn time: 150 s Specific impulse: 322 s (v) Vehicles: UR-200 (2 st.) First flight: 1967    RD-0207 Thrust: 775 kgf (v)

RD-0208 / 0209     Propellant: Thrust: 58,500 kgf (v) Specific impulse: 327 s (v)    3 x RD-0208 + 1 x RD-0209     Propellant: Vehicles: Proton (2  st.) First flight: 1965

RD-0210 / 0211     Propellant: Chamber pressure: 145 atmThrust: 59,357 kgf (v) Burn time:  230 s Specific impulse: 327 s (v)    3 x RD-0210 + 1 x RD-0211     Propellant: Vehicles: Proton (2 st.) First flight: 1967

RD-0212 (1 x RD-0213 + 4 x RD-0214)    RD-0213     Propellant: Chamber pressure: 145 atm Thrust: 62,508 kgf (v) Burn time:  230 s Specific impulse: 325 s (v) Vehicles: Proton (3 st.) First flight: 1967    RD-0214 Thrust: 787 kgf (v)

RD-0216     Propellant: Chamber pressure: 145 atm Thrust: 22,127 kgf (v) Thrust: 19,986 kgf (sl) Specific impulse: 279 s (v) Specific impulse: 312 s (sl) Vehicles: UR-100  (1 st.) First flight: 1965

RD-0233     Propellant: Chamber pressure: 198 atm Thrust: 52,617 kgf (v) Thrust: 47,722 kgf (sl) Burn time: 121 s Specific impulse: 285 s (v) Specific impulse: 310 s (sl) Vehicles: UR-100N(U)(1 st.) Vehicles: Strela, Rockot (1 st.) First flight: 1972

RD-268     Propellant: Chamber pressure: 222 atm Thrust: 125,425 kgf (v) Thrust: 116.859 kgf (sl) Burn time: 121 s Specific impulse: 296 s (v) Specific impulse: 319 s (sl) Vehicles:MR-UR-100(U) (1 st.) First flight: 1971

RD-264 (4x RD-263)     Propellant: Chamber pressure: 203 atm Thrust: 461,115 kgf (v) Thrust: 424,813 kgf (sl) Specific impulse: 293 s (v) Specific impulse: 318 s (sl) Vehicles:R-36M(U) (1 st.) First flight: 1977

15D13 (8D423)     Propellant: Thrust: 13,358 kgf (v) Burn time: 184 s Specific impulse: 325 s Vehicles: UR-100 (2 st.) First flight: 1965

RD-0235     Propellant: Chamber pressure: 169 atm Thrust:  24,473 kgf (v) Specific impulse:320 s (v) Vehicles: UR-100N(U) (2 st.) Vehicles: Strela, Rockot (2 st.) First flight: 1972    RD-0236     Thrust: 1,607 kgf (v)

RD-862     Propellant: Chamber pressure: 130 atm Thrust: 14,544 kgf (v) Burn time: 195 s Specific impulse: 331 s Vehicles: MR-UR-100(U) (2 st.) First flight: 1971

RD-857     Propellant: Chamber pressure: 126 atm Thrust: 14,000 kgf (v) Burn time: 215  s Specific impulse: 329 s Vehicles: RT-20 (2 st.) First flight: 1967

RD-0228     (1 x RD-0229 + 4 x RD-0230) Propellant: Thrust:  77,498 kgf (v) Specific impulse:340 s (v) Vehicles: R-36M(U) (2 st.) First flight: 1971    RD-0230    RD-0255     (1 x RD-0256 + 4 x RD-0257) Propellant: Chamber pressure: 161 atm Thrust:  85,248 kgf (v) Specific impulse:340 s (v) Vehicles: R-36M2 (2 st.) First flight: 1986    RD-0257

RD-0243     (1 x RD-0244 + 4 x RD-0245 Propellant: Chamber pressure: 266 atm Thrust: 69,544 kgf (v) Thrust: 63,018 kgf (sl) Burn time: 79 s Specific impulse: 288 s (v) Specific impulse: 321 s (sl) Vehicles: R-29 (1 st.) Vehicles: Volna, Shtil (1 st.) 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)

NK-9     Propellant: Chamber pressure: 77 atm Thrust: 45,000 kgf (v) Thrust: 36,750 kgf (sl) Specific impulse: 328 s (v) Specific impulse: 286 s (sl) Vehicles: GR-1

NK-9v     Propellant: Chamber pressure: 77 atm Thrust: 45,000 kgf (v) Specific impulse: 345 s (v) Vehicles: GR-1 (2 st.)    NK-19     Propellant: Chamber pressure: 91 atm Thrust: 46,000 kgf (v) Specific impulse: 345 s (v) Vehicles: N1 (3 st.) First flight: 1969

NK-21     Propellant: Chamber pressure: 91 atm Thrust: 40,992 kgf (v) Specific impulse: 340 s (v) Vehicles: N1 (3 st.) First flight: 1969    NK-39     Propellant: Chamber pressure: 91 atm Thrust: 41,706 kgf (v) Specific impulse: 352 s (v) Vehicles: N1F (3 st.)

NK-15     Propellant: Chamber pressure: 77 atm Thrust: 157,444 kgf (v) Thrust: 154,000 kgf (sl) Burn time: 113 s Specific impulse: 318 s (v) Specific impulse: 297 s (sl) Vehicles: N1  (1 st.) First flight: 1969

NK-15v     Propellant: Chamber pressure: 77 atm Thrust: 168,000 kgf (v) Specific impulse: 325 s (v) Vehicles: N1 (2  st.) First flight: 1969

NK-33     Propellant: Chamber pressure: 143 atm Thrust: 167,000 kgf (v) Thrust: 154,181 kgf (sl) Burn time: 600 s Specific impulse: 331 s (v) Specific impulse: 297 s (sl) Vehicles: N1F  (1 st.) First flight: unflown

NK-33     Propellant: Chamber pressure: 169 atm Thrust: 167,000 kgf (v) Thrust: 154,181 kgf (sl) Burn time: 600 s Specific impulse: 334 s (v) Specific impulse: 300 s (sl) Vehicles: Soyuz-2.1v  (1 st.) First flight: 2013

NK-33 (AJ26-62)     Propellant: Chamber pressure: 144 atm Thrust: 167,000 kgf (v) Thrust: 154,181 kgf (sl) Burn time: 600 s Specific impulse: 334 s (v) Specific impulse: 300 s (sl) Vehicles: Antares 1  (1 st.) First flight: 2013

NK-43     Propellant: Chamber pressure: 144 atm Thrust: 181,000 kgf (v) Thrust: 127,237 kgf (sl) Burn time: 600 s Specific impulse: 346 s (v) Specific impulse: 246 s (sl) Vehicles: N1F (2 st.) First flight: (unflown)    NK-43 (AJ26-60)     Vehicles: Kistler K-1

RD-170 / 170M     Propellant: Chamber pressure: 242 atm Thrust: 806.76 kgf (v) Thrust: 769,876 kgf (sl) Burn time: 150 s Specific impulse: 337 s (v) Specific impulse: 309 s (sl) Vehicles: Energia  (1 st.) First flight: 1985    RD-171 / 171M     Propellant: Chamber pressure: 242 atm Thrust: 769,876 kgf (sl) Burn time: 150 s Specific impulse: 337 s (v) Specific impulse: 309 s (sl) Vehicles: Zenit  (1 st.) First flight: 1985    RD-172     Propellant: Chamber pressure: 253 atm Thrust: 783,998 kgf (sl) Specific impulse: 337 s (v) Specific impulse: 310 s (sl) Vehicles: Vulkan  (1 st.) First flight: unflown

RD-180      Propellant: Chamber pressure: 263 atm Thrust: 423.386 kgf (sl) Burn time: 270 s Specific impulse: 339 s (v) Specific impulse: 313 s (sl) Vehicles: Atlas 3 / 5  (1 st.) First flight: 2000

RD-190     Propellant:    RD-191     Propellant: Chamber pressure: 254 atm Thrust: 212,000 kgf (sl) Burn time: 270 s Specific impulse: 337 s (v) Specific impulse: 311 s (sl) Vehicles: Angara, KSLV  (1 st.) First flight: 2009

RD-193     Propellant: Chamber pressure: 254 atm Thrust: 212,000 kgf (sl) Burn time: 270 s Specific impulse: 337 s (v) Specific impulse: 311 s (sl) Vehicles: Soyuz  (2 st.) First flight: unflown

RD-181     Propellant: Chamber pressure: 254 atm Thrust: 185,894 kgf (sl) Burn time: 270 s Specific impulse: 338 s (v) Specific impulse: 312 s (sl) Vehicles: Antares 2   (1 st.) First flight: 2013

RD-120     Propellant: Chamber pressure: 160 atm Thrust: 85,003 kgf (v) Burn time: 315  s Specific impulse: 350 s (v) Vehicles: Zenit 2 (2 st.)    First flight: 1985    RD-120     Propellant: Chamber pressure: 176 atm Thrust: 92,998 kgf (v) Specific impulse: 350 s (v) Vehicles: Zenit 3SL (2 st.)    First flight: 1999

RD-120U     Propellant: Chamber pressure: 159 atm 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: Chamber pressure: 159 atm Thrust: 89,408 kgf (v) Thrust: 79,303 kgf (sl) Burn time: 315  s Specific impulse: 340 s (v) Specific impulse: 301 s (sl) Vehicles: Soyuz-M  (2 st.)

RD-182     Propellant: Chamber pressure: 174 atm Thrust: 90,856 kgf (v) Thrust: 79,303 kgf (sl) Specific impulse: 353 s (v) Specific impulse: 316 s (sl)

YF-100     Propellant: Chamber pressure: 175 atm Thrust: 124,762 kgf (v) Thrust: 139,395 kgf(sl) Specific impulse: 335 s (v) Specific impulse: 300 s (sl) Vehicles: CZ-5 / 6 / 7  (1 st.) First flight: 2016

RD-810        SCE-200     Propellant: Chamber pressure: 178 atm Thrust: 214,548 kgf (v) Thrust: 191,298 kgf (sl) Specific impulse: 335 s (v) Specific impulse: 299 s (sl) Vehicles: ULV (LMV3) (1 st.)

YF-100K     Propellant: Chamber pressure: 178 atm Thrust: 125,527 kgf (v) Thrust: 140,312 kgf(sl) Specific impulse: 337 s (v) Specific impulse: 302 s (sl) Vehicles: CZ-5  (1 st.)

RD-58     Propellant: Thrust: 8.504 kgf (v) Chamber pressure: 76 atm Burn time: 600 s Specific impulse: 349 s (v) Vehicles: Proton  (Bl. D) Vehicles: N1  (Bl. D) First flight: 1967

RD-58 S     Propellant: Chamber pressure: 78 atm Thrust: 8,763 kgf (v) Burn time: 680 s Specific impulse: 361 s (v) Vehicles: Proton  (Bl. DM)

RD-58 M     Propellant: Chamber pressure: 76 atm Thrust: 8,668 kgf (v) Burn time: 600 s Burn time: 775 s Specific impulse: 356 s (v) Vehicles: Proton  (Bl. DM) First flight: 1974

17D12     Propellant: Chamber pressure: 76 atm Thrust: 8,800 kgf (v) Burn time: 680 s Specific impulse: 362 s (v) Vehicles: Buran   (OMS)

RD-58 Z  (carbon nozzle) Propellant: Chamber pressure: 76 atm Thrust: 8,102 kgf (v) Burn time: 640 s Burn time: 695 s Specific impulse: 361 s (v) Vehicles: Zenit  (Bl. DM)

RD-58 MFD

RD-58 MF     Propellant: Thrust: 5,007 kgf (v) Burn time: 1,400 s Specific impulse: 372 s (v)

RD-56 (KVD-1)     Propellant: Chamber pressure: 54 atm Thrust: 7,097 kgf (v) Burn time: 800 s Specific impulse: 462 s (v)    RD-56     Propellant: Chamber pressure: 54 atm Thrust: 7,097 kgf (v) Specific impulse: 462 s (v) Vehicles: GSLV Mk1 First flight: 1993

RD-0146     Propellant: Chamber pressure: 78 atm Thrust: 10,003 kgf (v) Burn time: 1100 s Specific impulse: 462 s (v)    RD-0146D     Propellant: Chamber pressure: 58 atm Thrust: 7,494 kgf (v) Specific impulse: 470 s (v) Vehicles: Angara-5V  (3 st.)    RD-0146E     Propellant: Chamber pressure: 78 atm Thrust: 10,003 kgf (v) Specific impulse: 470 s (v) Vehicles: Onega  (3 st.)

RD-0120     Propellant: Chamber pressure: 216 atm Thrust: 199,966 kgf (v) Thrust: 147,960 kgf (sl) Burn time: 600 s Specific impulse: 455 s (v) Specific impulse: 359 s (sl) Vehicles: Energia First flight: 1987

RD-0126     Propellant: Thrust:3,997 kgf (v) Chamber pressure: 58 atm Specific impulse: 470 s (v)

RD-0126E     Propellant: Thrust: 3,997 kgf (v) Chamber pressure: 68 atm Specific impulse: 472 s (v)

RD-161     Propellant: Chamber pressure: 116 atm Thrust: 2,000 kgf (v) Burn time: 900 s Specific impulse: 360 s (v)

RD-161     Propellant: Chamber pressure: 116 atm Thrust: 2,030 kgf (v) Burn time: 900 s Specific impulse: 365 s (v)

RD-119     Propellant: Chamber pressure: 78 atm Thrust: 10,758 kgf (v) Burn time: 260  s Specific impulse: 352 s (v) Vehicles: Kosmos  (2 st.) First flight: 1961

S 5.23 (11D49)     Propellant: Chamber pressure: 95 atm Thrust: 16,060 kgf (v) Burn time: 4,305 s Specific impulse: 303 s (v) Vehicles: Kosmos-3M  (2 st.) First flight: 1964

RD-854     Propellant: Chamber pressure: 84 atm Thrust: 7,698 kgf (v) Burn time: 70 s Specific impulse: 312 s Vehicles: R-36orb  (wh) First flight: 1962    RD-861     Propellant: Chamber pressure: 88 atm Thrust: 8,026 kgf (v) Burn time: 130 s Specific impulse: 317 s Vehicles: Tsiklon-2 / 3  (3 st.) First flight: 1965

s1.5400 (8D726)     Propellant: Chamber pressure: 52 atm Thrust: 6,801 kgf (v) Burn time: 208 s Vehicles: Molniya  (Bl. L) First flight: 1965

S 5.461     Propellant: Chamber pressure: 9 atm Thrust: 299 kgf (v) Specific impulse: 307 s (v) Vehicles: Soyuz (Bl. Ikar)

S 5.92     Propellant: Chamber pressure: 94 atm Thrust: 2,000 kgf (v) Burn time: 2,000 s Specific impulse: 327 s (v) Vehicles: Soyuz (Bl. Fregat) First flight: 2000

S 5.98M     Propellant: Thrust: 2,000 kgf (v) Burn time: 3,200 s Specific impulse: 326 s (v) Vehicles: Rokot, Proton-Briz M, Angara (Bl. Briz M) First flight: 1990

RD-866     Propellant: Thrust: 512 (v) Burn time: 330 s Specific impulse: 320 s Vehicles: RT-23, R-39 First flight: 1982

RD-869     Propellant: Thrust: 4 x 500 kgf (v) Burn time: 700 s Specific impulse: 320 s Vehicles: R-36M(U), Dnepr First flight: 1986