|
|
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-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-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-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 |
|
|
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 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 |
|
|
|
