2415:
273:
953:. Due to complexity of the technology involved in this type of engine, modifications or reverse engineering seem difficult to achieve. Thus it is believable that complete hardware could have been bought on black market and directly shipped to North Korea, by Russia or Ukraine. Conversely, there is analysis (made by two Ukrainian authors) suggesting an alternative mechanism for North Korea to receive
969:
38:
937:
Several experts think that technology from the RD-250 engine could have been transferred to North Korea from
Ukraine. This transfer would explain the rapid progress of North Korea in the development of two new missiles: the
2552:
2748:
2743:
2547:
1296:
1055:
2738:
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1370:
1319:
1401:
939:
1267:
1141:
1109:
2753:
2667:
946:
1343:
1238:
1077:
478:
Some of these engines were bundled into modules of multiple engines. The relevant modules and auxiliary engines are:
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151:
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2021:
1740:
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2082:
1411:
112:
1976:
2423:
1649:
1642:
1502:
1356:
2507:
2376:
2146:
2136:
1827:
1809:
17:
2048:
2692:
2642:
2562:
2522:
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2512:
2386:
2161:
2111:
2049:
1497:
2567:
1193:
1171:
2662:
2657:
2652:
2647:
2637:
2071:
1383:
690:
299:
122:
1716:
1709:
1338:
348:, but since the cancellation of the project it should be considered as out of production.
8:
2672:
2492:
2192:
2062:
1747:
1387:
2487:
1033:
292:
2617:
2597:
1323:
214:
203:
2016:
1434:
1991:
1971:
1966:
1961:
1585:
1422:
1390:
1378:
1275:
1246:
1149:
1117:
1085:
1059:
1028:
1024:
1010:
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996:
982:
954:
903:
897:
891:
530:
512:
494:
444:
408:
390:
372:
333:
322:
318:
243:
89:
66:
2732:
1996:
1780:
1696:
1622:
1441:
1379:
1214:
295:
974:
2086:
2053:
2712:* Different versions of the engine use different propellant combinations
2502:
2141:
1020:
950:
942:
272:
2477:
2472:
2121:
1014:
1006:
992:
915:
909:
552:
534:
466:
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97:
93:
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1875:
326:
193:
76:
1196:[Tsyklon - The second stage] (in French). Kosmonavtika.com
2677:
2232:
2227:
2222:
2217:
2212:
2207:
2202:
2197:
1917:
1880:
1870:
1865:
1839:
1728:
1615:
1560:
1554:
1174:[Tsyklon - The first stage] (in French). Kosmonavtika.com
932:
551:): A module comprising three RD-250PM. Propulsion module of the
2632:
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2006:
1950:
1943:
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1911:
1905:
1900:
1895:
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1820:
1814:
1804:
1680:
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1512:
1463:
529:): A module comprising three RD-250M. Propulsion module of the
511:): A module comprising three RD-250P. Propulsion module of the
493:): A module comprising three RD-250. Propulsion module of the
2682:
2622:
2451:
2446:
2441:
2436:
2397:
2391:
2335:
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2314:
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1344:
Encyclopedia
Astronautica information on RD-250 base engine.
957:
missile engines, or an entire missile, from USSR or Russia.
2319:
2309:
2101:
1937:
1776:
1691:
1590:
1579:
1538:
1532:
1527:
1492:
1215:"The RD-250 engine at the center of an international storm"
986:
593:
544:
522:
504:
486:
458:
436:
418:
400:
382:
364:
329:
284:
48:
2612:
2607:
2602:
2592:
37:
443:): Vacuum optimized version of the RD-250. Used on the
429:. A bundle of three RD-250PM form the RD-261 cluster.
411:. A bundle of three RD-250M form the RD-251M cluster.
393:. A bundle of three RD-250P form the RD-251P cluster.
964:
1772:
375:. A bundle of three RD-250 form the RD-251 cluster.
344:launch vehicles. It was supposed to be used on the
1322:, Mariana Budjeryn & Andrew Zhalko-Tytarenko,
291:) is the base version of a dual-nozzle family of
2730:
425:): Improved version of the RD-250M. Used on the
407:): Improved version of the RD-250P. Used on the
989:for which this engine was originally developed.
465:): Improved version of the RD-252. Used on the
389:): Improved version of the RD-250. Used on the
1320:North Korean Missile Engines: Not from Ukraine
1185:
1163:
933:Possible technological transfer to North Korea
1364:
1313:
356:The engine has seen different versions made:
336:(8K67). Its variations were also used on the
2749:Rocket engines using the gas-generator cycle
1339:Yuzhmash official information on the RD-261.
2744:Rocket engines using hypergolic propellant
1371:
1357:
1297:"The secret to North Korea's ICBM success"
1136:
1134:
1104:
1102:
1050:
1048:
371:): Base engine of the family. Used on the
36:
271:
1260:
1231:
1131:
1099:
1070:
1045:
14:
2731:
84:
1352:
1402:Comparison of orbital rocket engines
24:
2739:Rocket engines of the Soviet Union
1191:
1169:
947:intercontinental ballistic missile
714:8.924 MPa (1,294.3 psi)
711:8.336 MPa (1,209.0 psi)
25:
2770:
1332:
737:941.4 kN (211,600 lbf)
2413:
1056:"NPO Energomash list of engines"
967:
754:788.7 kN (177,300 lbf)
751:788.5 kN (177,300 lbf)
748:788.5 kN (177,300 lbf)
745:788.5 kN (177,300 lbf)
734:940.8 kN (211,500 lbf)
731:881.7 kN (198,200 lbf)
728:881.6 kN (198,200 lbf)
725:881.6 kN (198,200 lbf)
722:881.6 kN (198,200 lbf)
1289:
1034:Rocket engine using liquid fuel
1207:
1194:"Tsiklone - Le deuxième étage"
808:269.6 s (2.644 km/s)
784:317.6 s (3.115 km/s)
781:301.4 s (2.956 km/s)
317:. The RD-250 was developed by
198:8.33 MPa (1,208 psi)
187:788 kN (177,000 lbf)
179:882 kN (198,000 lbf)
13:
1:
2198:RD-0202 to 0206, 0208 to 0213
1172:"Tsiklone - Le premier étage"
1039:
559:
883:715 kg (1,576 lb)
860:2,590 mm (102 in)
787:318 s (3.12 km/s)
708:Combustion chamber pressure
7:
960:
880:715 kg (1,576 lb)
874:728 kg (1,605 lb)
871:728 kg (1,605 lb)
868:728 kg (1,605 lb)
857:2,590 mm (102 in)
837:2,190 mm (86 in)
828:2,600 mm (100 in)
825:2,600 mm (100 in)
822:2,600 mm (100 in)
778:301 s (2.95 km/s)
775:301 s (2.95 km/s)
772:301 s (2.95 km/s)
351:
233:788 kg (1,737 lb)
209:301 s (2.95 km/s)
10:
2775:
851:1,000 mm (39 in)
848:1,000 mm (39 in)
845:1,000 mm (39 in)
834:2,190 mm (86 in)
805:270 s (2.6 km/s)
802:270 s (2.6 km/s)
799:270 s (2.6 km/s)
473:
220:270 s (2.6 km/s)
2754:Energomash rocket engines
2708:
2422:
2411:
2351:
2041:
1763:
1611:
1430:
1421:
1410:
1397:
1272:Encyclopedia Astronautica
1243:Encyclopedia Astronautica
1146:Encyclopedia Astronautica
1114:Encyclopedia Astronautica
1082:Encyclopedia Astronautica
713:
710:
689:
565:RD-250 Family of Engines
263:
258:
242:
237:
229:
224:
213:
202:
191:
183:
175:
170:
162:
157:
147:
139:
118:
111:
103:
82:
72:
62:
54:
44:
35:
315:gas-generator open cycle
2759:Yuzhmash rocket engines
2243:RD-250 to 252, 261, 262
1219:www.russianspaceweb.com
276:
2719:are under development
2107:YF-20, 21, 22, 24, 25
1886:RD-107, 108, 117, 118
275:
926:Tsyklon-3 2nd stage
2208:RD-0216, 0217, 0235
1871:RD-0107, 0108, 0110
1249:on October 28, 2002
1066:on 7 November 2014.
1013:developed from the
923:Tsyklon-2 2nd stage
921:R-36, R36P, R-36-O,
566:
515:(8K68) first stage.
497:(8K67) first stage.
58:December 16th, 1965
32:
1088:on August 26, 2002
940:intermediate-range
742:Thrust, sea level
564:
277:
113:Liquid-fuel engine
30:
2726:
2725:
2668:Space Shuttle SRB
2409:
2408:
2347:
2346:
2037:
2036:
1759:
1758:
1192:Pillet, Nicolas.
1170:Pillet, Nicolas.
930:
929:
900:(8K67P) 1st stage
270:
269:
184:Thrust, sea-level
107:Out of Production
45:Country of origin
16:(Redirected from
2766:
2417:
2416:
2253:RD-263, 268, 273
2184:along other LREs
2046:
2045:
1906:RD-191, 151, 181
1770:
1769:
1428:
1427:
1419:
1418:
1373:
1366:
1359:
1350:
1349:
1327:
1324:Atlantic Council
1317:
1311:
1310:
1308:
1307:
1293:
1287:
1286:
1284:
1283:
1278:on June 27, 2002
1274:. Archived from
1264:
1258:
1257:
1255:
1254:
1245:. Archived from
1235:
1229:
1228:
1226:
1225:
1211:
1205:
1204:
1202:
1201:
1189:
1183:
1182:
1180:
1179:
1167:
1161:
1160:
1158:
1157:
1148:. Archived from
1138:
1129:
1128:
1126:
1125:
1120:on June 26, 2002
1116:. Archived from
1106:
1097:
1096:
1094:
1093:
1084:. Archived from
1074:
1068:
1067:
1062:. Archived from
1052:
977:
972:
971:
970:
894:(8K67) 1st stage
567:
563:
215:Specific impulse
204:Specific impulse
86:
40:
33:
31:RD-250 (РД-250)
29:
21:
2774:
2773:
2769:
2768:
2767:
2765:
2764:
2763:
2729:
2728:
2727:
2722:
2704:
2425:
2418:
2414:
2405:
2343:
2233:RD-0255 to 0257
2228:RD-0243 to 0245
2090:
2079:
2075:
2069:
2057:
2033:
1774:
1765:
1755:
1619:
1613:
1607:
1438:
1432:
1413:
1406:
1393:
1391:launch vehicles
1377:
1335:
1330:
1318:
1314:
1305:
1303:
1295:
1294:
1290:
1281:
1279:
1266:
1265:
1261:
1252:
1250:
1237:
1236:
1232:
1223:
1221:
1213:
1212:
1208:
1199:
1197:
1190:
1186:
1177:
1175:
1168:
1164:
1155:
1153:
1152:on May 31, 2002
1140:
1139:
1132:
1123:
1121:
1108:
1107:
1100:
1091:
1089:
1076:
1075:
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1053:
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1042:
973:
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963:
935:
922:
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795:
768:
719:Thrust, vacuum
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694:
562:
476:
354:
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28:
23:
22:
15:
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1992:LR70-NA , S-3D
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1380:Rocket engines
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1060:NPO Energomash
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1038:
1037:
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1031:
1025:launch vehicle
1018:
1011:launch vehicle
1009:- Three stage
1004:
997:launch vehicle
990:
983:R-36 (missile)
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296:rocket engines
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2367:RD-211 to 214
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2213:RD-0233, 0234
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2203:RD-0207, 0214
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2182:Paektusan LRE
2180:
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1866:RD-0105, 0109
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1550:KVD-1 (RD-56)
1548:
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1027:based on the
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1005:
1002:
999:based on the
998:
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216:
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205:
201:
197:
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190:
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182:
178:
174:
169:
165:
161:
158:Configuration
156:
153:
152:Gas-generator
150:
146:
142:
140:Mixture ratio
138:
135:
131:
121:
117:
114:
110:
106:
102:
99:
95:
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88:
81:
78:
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68:
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61:
57:
53:
50:
47:
43:
39:
34:
27:Rocket engine
19:
2716:
2257:
2242:
2181:
2178:North Korea
1949:
1942:
1910:
1838:
1826:
1819:
1797:
1746:
1739:
1727:
1715:
1708:
1701:
1679:
1672:
1665:
1648:
1641:
1634:
1578:
1571:
1559:
1537:
1480:
1473:
1384:solid motors
1326:, 2017-09-12
1315:
1304:. Retrieved
1301:www.iiss.org
1300:
1291:
1280:. Retrieved
1276:the original
1271:
1262:
1251:. Retrieved
1247:the original
1242:
1233:
1222:. Retrieved
1218:
1209:
1198:. Retrieved
1187:
1176:. Retrieved
1165:
1154:. Retrieved
1150:the original
1145:
1122:. Retrieved
1118:the original
1113:
1090:. Retrieved
1086:the original
1081:
1072:
1064:the original
975:Space portal
936:
796:, sea level
664:Development
641:Module GRAU
555:first stage.
548:
540:
537:first stage.
526:
518:
508:
500:
490:
482:
477:
462:
454:
440:
432:
422:
414:
404:
396:
386:
378:
368:
360:
355:
288:
280:
278:
73:Manufacturer
55:First flight
2715:Engines in
2362:RD-109, 119
2300:RD-864, 869
2285:RD-854, 861
2248:RD-253, 275
1896:RD-170, 171
865:Dry weight
687:Propellant
533:(8K69) and
327:PA Yuzhmash
254:first stage
217:, sea-level
171:Performance
83:Associated
77:PA Yuzhmash
2733:Categories
2102:YF-1, 2, 3
2050:Hypergolic
2022:Rutherford
1741:Prometheus
1703:Archimedes
1306:2017-08-15
1282:2015-06-20
1253:2015-06-20
1224:2023-01-03
1200:2016-07-04
1178:2016-07-04
1156:2015-06-20
1124:2015-06-20
1092:2015-06-20
1040:References
1021:Cyclone-4M
951:Hwasong-14
943:Hwasong-12
682:1968-1970
560:Comparison
298:, burning
264:References
259:References
225:Dimensions
119:Propellant
2643:Castor 30
2523:Zefiro 40
2518:Zefiro 23
2459:SpaB-140C
1856:NK-33, 44
1766:cryogenic
1612:Methalox
1431:Hydrolox
1423:Cryogenic
1015:Tsyklon-2
1007:Tsyklon-3
993:Tsyklon-2
918:1st stage
916:Tsyklon-3
912:1st stage
910:Tsyklon-2
842:Diameter
769:, vacuum
679:1962-1966
676:1968-1970
673:1966-1968
670:1967-1968
667:1962-1966
582:RD-250PM
553:Tsyklon-3
535:Tsyklon-2
467:Tsyklon-3
449:Tsyklon-2
427:Tsyklon-3
346:Tsyklon-4
342:Tsyklon-3
338:Tsyklon-2
252:Tsyklon-3
248:Tsyklon-2
98:Tsyklon-3
94:Tsyklon-2
2658:Orbus-21
2513:Zefiro 9
2276:Ukraine
2054:Aerozine
2042:Storable
1934:Ukraine
1876:RD-0110R
1773:Kerolox
1268:"RD-261"
1239:"RD-262"
1142:"RD-252"
1110:"RD-251"
1078:"RD-250"
961:See also
949:(ICBM),
945:and the
906:(8K67-O)
579:RD-250M
576:RD-250P
415:RD-250PM
352:Versions
230:Dry mass
206:, vacuum
194:pressure
192:Chamber
63:Designer
2717:italics
2678:Star 48
2673:Star 37
2653:Orbus-6
2574:Israel
2508:Waxwing
2464:Europe
2456:SpaB-65
2358:Russia
2223:RD-0237
2218:RD-0236
2189:Russia
2168:Israel
2128:Europe
1972:Kestrel
1918:S1.5400
1881:RD-0124
1847:Russia
1840:SCE-200
1736:Europe
1729:RD-0169
1724:Russia
1650:Longyun
1643:Lingyun
1561:RD-0146
1555:RD-0120
1546:Russia
1503:Vulcain
1489:Europe
1412:Liquid
1388:orbital
819:Length
627:RD-251M
624:RD-251P
618:Module
607:8D518PM
588:RD-262
585:RD-252
573:RD-250
570:Engine
519:RD-251M
501:RD-251P
474:Modules
423:8D518PM
397:RD-250M
379:RD-250P
319:OKB-456
313:in the
238:Used in
163:Chamber
67:OKB-456
2633:AJ-60A
2598:KM-V2b
2589:Japan
2563:Salman
2529:India
2503:Topaze
2468:Mage 1
2433:China
2424:Solid
2331:TR-201
2295:RD-856
2290:RD-855
2280:RD-843
2270:S5.98M
2259:RD-270
2153:India
2147:Viking
2137:Astris
2132:Aestus
2122:YF-50D
2098:China
2007:RS-27A
1997:Merlin
1987:LR-105
1951:RD-810
1944:RD-801
1928:TEPREL
1924:Spain
1912:RD-193
1901:RD-180
1891:RD-120
1835:India
1828:Welkin
1821:YF-130
1815:YF-115
1810:YF-102
1805:YF-100
1789:China
1717:Aeon R
1710:Aeon 1
1697:Raptor
1681:YF-215
1674:YF-209
1667:TQ-15A
1631:China
1524:Japan
1513:CE-7.5
1509:India
1464:YF-75D
1450:China
904:R-36-O
650:8D723M
647:8D723P
630:RD-261
621:RD-251
613:11D26
604:8D518M
601:8D518P
547:Index
541:RD-261
531:R-36-O
527:8D723M
525:Index
509:8D723P
507:Index
489:Index
483:RD-251
461:Index
455:RD-262
439:Index
433:RD-252
421:Index
409:R-36-O
405:8D518M
403:Index
387:8D518P
385:Index
367:Index
361:RD-250
332:, the
323:Yangel
293:liquid
287:Index
281:RD-250
104:Status
18:RD-262
2698:X-254
2693:X-248
2683:UA120
2663:Orion
2638:Algol
2623:SRB-A
2618:M-34c
2593:KM-V1
2583:RSA-3
2559:Iran
2452:FG-47
2447:FG-46
2442:FG-36
2437:FG-02
2398:XLR81
2392:RS-88
2387:Curie
2377:Gamma
2352:Other
2336:XLR81
2325:RS-88
2320:LR-91
2315:LR-87
2265:S5.92
2193:17D61
2162:Vikas
2142:Vexin
2117:YF-40
2112:YF-23
2085:, or
2065:, or
2059:UH 25
2027:XLR50
2012:RS-56
2002:RS-27
1982:LR-89
1977:LR-79
1861:RD-58
1851:NK-15
1799:TH-12
1793:TH-11
1764:Semi-
1661:TQ-12
1656:TQ-11
1636:BF-20
1601:RS-68
1596:RS-25
1573:BE-3U
1518:CE-20
1498:Vinci
1482:YF-90
1475:YF-79
1469:YF-77
1459:YF-75
1454:YF-73
898:R-36P
653:11D69
644:8D723
610:8D724
598:8D518
549:11D69
513:R-36P
491:8D723
463:11D26
441:8D724
391:R-36P
369:8D518
289:8D518
148:Cycle
2688:SRMU
2613:M-34
2608:M-24
2603:M-14
2578:LK-1
2568:Rafe
2553:S200
2548:S139
2498:P230
2493:P120
2426:fuel
2310:AJ10
2172:LK-4
2067:UDMH
2017:S-3D
1938:RD-8
1777:RP-1
1748:M-10
1692:BE-4
1591:RL10
1580:BE-7
1539:LE-9
1533:LE-7
1528:LE-5
1493:HM7B
1414:fuel
1386:for
1382:and
1029:R-36
1001:R-36
987:ICBM
955:R-36
908:and
892:R-36
888:Use
814:N/A
760:N/A
702:UDMH
659:N/A
636:N/A
594:GRAU
545:GRAU
523:GRAU
505:GRAU
495:R-36
487:GRAU
459:GRAU
447:and
445:R-36
437:GRAU
419:GRAU
401:GRAU
383:GRAU
373:R-36
365:GRAU
340:and
334:R-36
330:ICBM
321:for
311:UDMH
309:and
285:GRAU
279:The
250:and
244:R-36
134:UDMH
96:and
90:R-36
49:USSR
2648:GEM
2543:S12
2488:P80
2483:PAP
2478:P-6
2473:P-4
2373:UK
2157:PS4
2087:HNO
2083:MON
2063:MMH
1967:H-1
1962:F-1
1781:LOX
1623:LOX
1586:J-2
1442:LOX
877:N/A
854:N/A
831:N/A
811:N/A
757:N/A
656:N/A
633:N/A
325:'s
143:2.6
2735::
2538:S9
2533:S7
2081:,
2070:/
2061:,
2056:,
1779:/
1621:/
1616:CH
1440:/
1435:LH
1299:.
1270:.
1241:.
1217:.
1144:.
1133:^
1112:.
1101:^
1080:.
1058:.
1047:^
1023:-
995:-
985:-
794:sp
767:sp
246:,
132:/
92:,
85:LV
2400:*
2394:*
2338:*
2327:*
2092:)
2089:3
2078:4
2076:O
2074:2
2072:N
2052:(
1783:)
1775:(
1625:)
1618:4
1614:(
1444:)
1437:2
1433:(
1372:e
1365:t
1358:v
1309:.
1285:.
1256:.
1227:.
1203:.
1181:.
1159:.
1127:.
1095:.
1017:.
1003:.
792:I
765:I
700:/
697:4
695:O
693:2
691:N
543:(
521:(
503:(
485:(
457:(
435:(
417:(
399:(
381:(
363:(
306:4
304:O
302:2
300:N
283:(
166:2
129:4
127:O
125:2
123:N
20:)
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