2313:
755:
350:
development. By April 1970 Yuzhnoye was getting the engine documentation. By the end of 1972 Energomash started to test fire the engines in its own test stand. And by
September 1973 the engine was certified for flight. While the engine is out of production, the
2646:
2641:
2450:
2636:
1268:
2445:
924:
1299:
2651:
2565:
2656:
498:
320:
142:
1964:
513:
316:
124:
2440:
2435:
2430:
2054:
1230:
1146:
1040:
1238:
1061:
1199:
1093:
981:
1261:
949:
858:
705:
Some of these engines were bundled into modules of multiple engines. The relevant modules and auxiliary engines are:
2585:
1919:
1638:
1600:
1980:
1309:
495:
103:
1246:
2321:
1547:
1540:
1400:
1254:
1175:
2405:
2274:
2044:
2034:
1725:
1707:
339:
2595:
2590:
2540:
2460:
2420:
2415:
2410:
2284:
2059:
2009:
1947:
1395:
796:
932:
2560:
2555:
2550:
2545:
2535:
1969:
1281:
502:
305:
113:
2570:
2390:
2090:
1960:
1645:
1285:
2385:
802:
298:
2465:
2515:
2495:
1614:
1607:
205:
194:
61:
1914:
1332:
216:
1889:
1869:
1864:
1859:
1483:
1320:
1288:
928:
786:
782:
778:
768:
739:
725:
721:
670:
654:
650:
423:
387:
383:
356:
352:
343:
336:
264:
260:
88:
84:
57:
1016:
2630:
1894:
1678:
1594:
1520:
1339:
1277:
664:
660:
409:
405:
301:
760:
1154:
1044:
1984:
1951:
1884:
1879:
1874:
1069:
1207:
1101:
989:
957:
866:
750:
422:): Improved version based on the RD-263F upgrade project. Version used on the
2019:
891:
825:
2480:
2475:
2395:
2380:
2365:
2069:
1773:
184:
71:
2610:* Different versions of the engine use different propellant combinations
2575:
2400:
2375:
2370:
2130:
2125:
2120:
2115:
2110:
2105:
2100:
2095:
2039:
1815:
1778:
1768:
1763:
1737:
1626:
1513:
1458:
1452:
17:
2530:
2264:
2259:
2228:
2197:
2192:
2187:
2182:
2177:
2167:
2156:
2145:
2140:
2135:
2079:
2029:
1904:
1848:
1841:
1825:
1809:
1803:
1798:
1793:
1788:
1783:
1718:
1712:
1702:
1578:
1571:
1410:
1361:
1127:
Lardier, Christian. "Liquid
Propellant Engines in the Soviet Union".
347:
346:, instead of both stages, arguing that they were overworked with the
738:
Index ): A module comprising four RD-273. Propulsion module of the
2580:
2520:
2349:
2344:
2339:
2334:
2295:
2289:
2233:
2222:
2212:
2162:
2014:
2004:
1956:
1924:
1909:
1899:
1758:
1753:
1748:
1696:
1690:
1564:
1558:
1553:
1533:
1498:
1493:
1470:
1447:
1415:
1379:
1372:
1366:
1356:
1351:
792:
2217:
2207:
1999:
1835:
1674:
1589:
1488:
1477:
1436:
1430:
1425:
1390:
1239:
Encyclopedia
Astronautica information on the propulsion module.
772:
735:
713:
397:
375:
328:
290:
39:
1250:
2510:
2505:
2500:
2490:
720:): A module comprising four RD-263. Propulsion module of the
795:, twin-chamber American rocket engine family used on the
323:
cycle. Four RD-263 engines form a propulsion module
2320:
2249:
1946:
1939:
1670:
1661:
1509:
1328:
1319:
1308:
276:
271:
254:
246:
238:
230:
225:
215:
204:
193:
182:
174:
166:
161:
153:
148:
138:
130:
109:
102:
94:
77:
67:
53:
45:
35:
2647:Rocket engines using the staged combustion cycle
1122:
1120:
1118:
1010:
1008:
1006:
775:for which this engine was originally developed.
1262:
8:
30:
1088:
1086:
1056:
1054:
885:
883:
342:only ordered the first stage propulsion to
2642:Rocket engines using hypergolic propellant
1943:
1667:
1325:
1316:
1269:
1255:
1247:
1231:KbKhA official information on the engine.
976:
974:
944:
942:
919:
917:
915:
913:
911:
853:
851:
849:
847:
845:
819:
817:
1181:. Nuclear Threat Initiative. August 2012
1135:. American Astronautical Society: 39–73.
429:
813:
367:The basic engine has been used for the
79:
29:
516:propellant with an O/F ratio of 2.67
7:
1300:Comparison of orbital rocket engines
178:1,040 kilonewtons (230,000 lbf)
170:1,128 kilonewtons (254,000 lbf)
742:(15A18M) and (15A18M2) first stage.
673:(15A18M) and (15A18M2) first stage
426:(15A18M) and (15A18M2) first stage.
2637:Rocket engines of the Soviet Union
25:
1129:Thirty-third IAA History Simposia
558:1,130 kN (250,000 lbf)
544:1,240 kN (280,000 lbf)
189:20.6 megapascals (2,990 psi)
2311:
1153:. Missile Threat. Archived from
1043:. NPO Energomash. Archived from
925:"NPO Energomash list of engines"
753:
555:1,130 kN (250,000 lbf)
552:1,040 kN (230,000 lbf)
541:1,240 kN (280,000 lbf)
538:1,130 kN (250,000 lbf)
826:"R-36M/15A14/SS-18/Satan/RS-20"
803:Rocket engine using liquid fuel
530:22.6 MPa (3,280 psi)
499:oxidizer rich staged combustion
382:): Initial version used on the
359:remain operational as of 2015.
321:oxidizer rich staged combustion
143:Oxidizer-rich staged combustion
728:first stage (15А14 and 15A18).
527:22.6 MPa (3,280 psi)
524:20.6 MPa (2,990 psi)
390:first stage (15А14 and 15A18).
242:1,080 millimetres (43 in)
234:2,150 millimetres (85 in)
1:
2096:RD-0202 to 0206, 0208 to 0213
250:870 kilograms (1,920 lb)
623:1,083 mm (42.6 in)
521:Combustion chamber pressure
267:core stage (15А14 and 15A18)
637:770 kg (1,700 lb)
634:870 kg (1,920 lb)
626:1,080 mm (43 in)
612:2,150 mm (85 in)
211:293 s (2.87 km/s)
200:318 s (3.12 km/s)
2673:
620:1,080 mm (43 in)
609:2,150 mm (85 in)
606:2,150 mm (85 in)
431:RD-0210 family of engines
2652:Energomash rocket engines
2606:
2309:
1295:
1204:Encyclopedia Astronautica
1098:Encyclopedia Astronautica
1066:Encyclopedia Astronautica
986:Encyclopedia Astronautica
954:Encyclopedia Astronautica
863:Encyclopedia Astronautica
694:
494:
404:): Variation used on the
259:
2657:Yuzhmash rocket engines
2141:RD-250 to 252, 261, 262
1021:Jonathan's Space Report
799:of US launch vehicles.
2617:are under development
2005:YF-20, 21, 22, 24, 25
1784:RD-107, 108, 117, 118
1176:"Kazakhstan Missiles"
785:that is a repurposed
1147:"Ballistic Missiles"
1015:McDowell, Jonathan.
892:"The Dnepr launcher"
412:(15A16) first stage.
2106:RD-0216, 0217, 0235
1769:RD-0107, 0108, 0110
935:on 7 November 2014.
896:RussianSpaceWeb.com
869:on January 13, 2003
830:RussianSpaceWeb.com
667:(15A16) first stage
432:
32:
657:(15A18) core stage
549:Thrust, sea level
464:Propulsion module
430:
104:Liquid-fuel engine
2624:
2623:
2566:Space Shuttle SRB
2307:
2306:
2245:
2244:
1935:
1934:
1657:
1656:
1151:missilethreat.com
1047:on 21 March 2016.
1017:"Russian engines"
698:
697:
681:Out of production
283:
282:
175:Thrust, sea-level
98:Out of production
36:Country of origin
16:(Redirected from
2664:
2315:
2314:
2151:RD-263, 268, 273
2082:along other LREs
1944:
1804:RD-191, 151, 181
1668:
1326:
1317:
1271:
1264:
1257:
1248:
1219:
1218:
1216:
1215:
1206:. Archived from
1196:
1190:
1189:
1187:
1186:
1180:
1172:
1166:
1165:
1163:
1162:
1143:
1137:
1136:
1124:
1113:
1112:
1110:
1109:
1100:. Archived from
1090:
1081:
1080:
1078:
1077:
1068:. Archived from
1058:
1049:
1048:
1037:
1031:
1030:
1028:
1027:
1012:
1001:
1000:
998:
997:
988:. Archived from
978:
969:
968:
966:
965:
956:. Archived from
946:
937:
936:
931:. Archived from
921:
906:
905:
903:
902:
887:
878:
877:
875:
874:
865:. Archived from
855:
840:
839:
837:
836:
821:
763:
758:
757:
756:
433:
206:Specific impulse
195:Specific impulse
81:
33:
31:RD-263 (РД-263)
21:
2672:
2671:
2667:
2666:
2665:
2663:
2662:
2661:
2627:
2626:
2625:
2620:
2602:
2323:
2316:
2312:
2303:
2241:
2131:RD-0255 to 0257
2126:RD-0243 to 0245
1988:
1977:
1973:
1967:
1955:
1931:
1672:
1663:
1653:
1517:
1511:
1505:
1336:
1330:
1311:
1304:
1291:
1289:launch vehicles
1275:
1227:
1222:
1213:
1211:
1198:
1197:
1193:
1184:
1182:
1178:
1174:
1173:
1169:
1160:
1158:
1145:
1144:
1140:
1126:
1125:
1116:
1107:
1105:
1092:
1091:
1084:
1075:
1073:
1072:on May 31, 2002
1060:
1059:
1052:
1039:
1038:
1034:
1025:
1023:
1014:
1013:
1004:
995:
993:
980:
979:
972:
963:
961:
948:
947:
940:
923:
922:
909:
900:
898:
889:
888:
881:
872:
870:
857:
856:
843:
834:
832:
823:
822:
815:
811:
759:
754:
752:
749:
703:
588:
568:
535:Thrust, vacuum
510:
506:
365:
355:as well as the
313:
309:
121:
117:
28:
23:
22:
15:
12:
11:
5:
2670:
2668:
2660:
2659:
2654:
2649:
2644:
2639:
2629:
2628:
2622:
2621:
2619:
2618:
2611:
2607:
2604:
2603:
2601:
2600:
2599:
2598:
2593:
2588:
2583:
2578:
2573:
2568:
2563:
2558:
2553:
2548:
2543:
2538:
2533:
2527:United States
2525:
2524:
2523:
2518:
2513:
2508:
2503:
2498:
2493:
2485:
2484:
2483:
2478:
2470:
2469:
2468:
2463:
2455:
2454:
2453:
2448:
2443:
2438:
2433:
2425:
2424:
2423:
2418:
2413:
2408:
2403:
2398:
2393:
2388:
2383:
2378:
2373:
2368:
2360:
2359:
2358:
2355:
2352:
2347:
2342:
2337:
2328:
2326:
2318:
2317:
2310:
2308:
2305:
2304:
2302:
2301:
2300:
2299:
2293:
2287:
2281:United States
2279:
2278:
2277:
2269:
2268:
2267:
2262:
2253:
2251:
2247:
2246:
2243:
2242:
2240:
2239:
2238:
2237:
2231:
2226:
2220:
2215:
2210:
2204:United States
2202:
2201:
2200:
2195:
2190:
2185:
2180:
2172:
2171:
2170:
2165:
2160:
2153:
2148:
2143:
2138:
2133:
2128:
2123:
2118:
2113:
2108:
2103:
2098:
2093:
2085:
2084:
2083:
2074:
2073:
2072:
2064:
2063:
2062:
2057:
2049:
2048:
2047:
2042:
2037:
2032:
2024:
2023:
2022:
2017:
2012:
2007:
2002:
1993:
1991:
1986:
1975:
1971:
1941:
1937:
1936:
1933:
1932:
1930:
1929:
1928:
1927:
1922:
1917:
1912:
1907:
1902:
1897:
1892:
1890:LR70-NA , S-3D
1887:
1882:
1877:
1872:
1867:
1862:
1856:United States
1854:
1853:
1852:
1845:
1838:
1830:
1829:
1828:
1820:
1819:
1818:
1813:
1806:
1801:
1796:
1791:
1786:
1781:
1776:
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1742:
1741:
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1715:
1710:
1705:
1700:
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1665:
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1655:
1654:
1652:
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1650:
1649:
1642:
1632:
1631:
1630:
1620:
1619:
1618:
1611:
1604:
1597:
1592:
1586:United States
1584:
1583:
1582:
1575:
1568:
1561:
1556:
1551:
1544:
1537:
1526:
1524:
1515:
1507:
1506:
1504:
1503:
1502:
1501:
1496:
1491:
1486:
1481:
1474:
1466:United States
1464:
1463:
1462:
1455:
1450:
1442:
1441:
1440:
1433:
1428:
1420:
1419:
1418:
1413:
1405:
1404:
1403:
1398:
1393:
1385:
1384:
1383:
1376:
1369:
1364:
1359:
1354:
1345:
1343:
1334:
1323:
1314:
1306:
1305:
1303:
1302:
1296:
1293:
1292:
1278:Rocket engines
1276:
1274:
1273:
1266:
1259:
1251:
1245:
1244:
1236:
1226:
1225:External links
1223:
1221:
1220:
1210:on May 6, 2002
1191:
1167:
1138:
1114:
1104:on May 6, 2002
1082:
1050:
1032:
1002:
970:
938:
929:NPO Energomash
907:
890:Zak, Anatoly.
879:
841:
824:Zak, Anatoly.
812:
810:
807:
806:
805:
800:
790:
783:launch vehicle
776:
765:
764:
748:
745:
744:
743:
729:
702:
699:
696:
695:
693:
689:
688:
685:
682:
679:
675:
674:
668:
665:MR-UR-100UTTKh
658:
648:
644:
643:
638:
635:
632:
628:
627:
624:
621:
618:
614:
613:
610:
607:
604:
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579:
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570:
566:
560:
559:
556:
553:
550:
546:
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542:
539:
536:
532:
531:
528:
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508:
504:
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482:
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468:
465:
461:
460:
457:
454:
451:
447:
446:
443:
440:
437:
428:
427:
413:
410:MR-UR-100UTTKh
391:
364:
361:
311:
307:
281:
280:
278:
274:
273:
269:
268:
257:
256:
252:
251:
248:
244:
243:
240:
236:
235:
232:
228:
227:
223:
222:
219:
213:
212:
209:
202:
201:
198:
191:
190:
187:
180:
179:
176:
172:
171:
168:
167:Thrust, vacuum
164:
163:
159:
158:
155:
151:
150:
146:
145:
140:
136:
135:
132:
128:
127:
119:
115:
111:
107:
106:
100:
99:
96:
92:
91:
82:
75:
74:
69:
65:
64:
55:
51:
50:
47:
43:
42:
37:
26:
24:
14:
13:
10:
9:
6:
4:
3:
2:
2669:
2658:
2655:
2653:
2650:
2648:
2645:
2643:
2640:
2638:
2635:
2634:
2632:
2616:
2612:
2609:
2608:
2605:
2597:
2594:
2592:
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2534:
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2529:
2528:
2526:
2522:
2519:
2517:
2514:
2512:
2509:
2507:
2504:
2502:
2499:
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2494:
2492:
2489:
2488:
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2482:
2479:
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2473:
2471:
2467:
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2456:
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2449:
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2442:
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2437:
2434:
2432:
2429:
2428:
2426:
2422:
2419:
2417:
2414:
2412:
2409:
2407:
2404:
2402:
2399:
2397:
2394:
2392:
2389:
2387:
2384:
2382:
2379:
2377:
2374:
2372:
2369:
2367:
2364:
2363:
2361:
2356:
2353:
2351:
2348:
2346:
2343:
2341:
2338:
2336:
2333:
2332:
2330:
2329:
2327:
2325:
2319:
2297:
2294:
2291:
2288:
2286:
2283:
2282:
2280:
2276:
2273:
2272:
2270:
2266:
2265:RD-211 to 214
2263:
2261:
2258:
2257:
2255:
2254:
2252:
2248:
2235:
2232:
2230:
2227:
2224:
2221:
2219:
2216:
2214:
2211:
2209:
2206:
2205:
2203:
2199:
2196:
2194:
2191:
2189:
2186:
2184:
2181:
2179:
2176:
2175:
2173:
2169:
2166:
2164:
2161:
2159:
2158:
2154:
2152:
2149:
2147:
2144:
2142:
2139:
2137:
2136:RD-215 to 219
2134:
2132:
2129:
2127:
2124:
2122:
2119:
2117:
2114:
2112:
2111:RD-0233, 0234
2109:
2107:
2104:
2102:
2101:RD-0207, 0214
2099:
2097:
2094:
2092:
2089:
2088:
2086:
2081:
2080:Paektusan LRE
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1448:KVD-1 (RD-56)
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1157:on 2014-08-22
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1003:
992:on 2015-08-24
991:
987:
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960:on 2016-03-27
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322:
318:
314:
303:
302:rocket engine
300:
296:
292:
288:
279:
275:
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266:
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156:
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149:Configuration
147:
144:
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137:
133:
131:Mixture ratio
129:
126:
122:
112:
108:
105:
101:
97:
93:
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66:
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48:
44:
41:
38:
34:
27:Rocket engine
19:
2614:
2155:
2150:
2076:North Korea
1847:
1840:
1808:
1736:
1724:
1717:
1695:
1644:
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1625:
1613:
1606:
1599:
1577:
1570:
1563:
1546:
1539:
1532:
1476:
1469:
1457:
1435:
1378:
1371:
1282:solid motors
1240:
1232:
1212:. Retrieved
1208:the original
1203:
1194:
1183:. Retrieved
1170:
1159:. Retrieved
1155:the original
1150:
1141:
1132:
1128:
1106:. Retrieved
1102:the original
1097:
1074:. Retrieved
1070:the original
1065:
1045:the original
1035:
1024:. Retrieved
1020:
994:. Retrieved
990:the original
985:
962:. Retrieved
958:the original
953:
933:the original
899:. Retrieved
895:
871:. Retrieved
867:the original
862:
833:. Retrieved
829:
797:Titan series
761:Space portal
731:
717:
709:
704:
663:(15А15) and
653:(15А14) and
640:
589:, sea level
583:
563:
492:Engine type
478:Development
419:
415:
408:(15А15) and
401:
393:
379:
371:
366:
332:
324:
294:
286:
284:
217:Gimbal range
68:Manufacturer
2613:Engines in
2260:RD-109, 119
2198:RD-864, 869
2183:RD-854, 861
2146:RD-253, 275
1794:RD-170, 171
692:References
631:Dry weight
340:KB Yuzhnoye
335:). For the
208:, sea-level
162:Performance
78:Associated
72:PA Yuzhmash
2631:Categories
2000:YF-1, 2, 3
1948:Hypergolic
1920:Rutherford
1639:Prometheus
1601:Archimedes
1241:(Archived)
1233:(Archived)
1214:2015-07-24
1185:2015-07-24
1161:2015-07-24
1108:2015-07-24
1076:2015-07-24
1026:2015-07-24
996:2015-07-24
964:2015-06-20
901:2015-06-20
873:2015-06-20
835:2015-06-20
809:References
787:R-36MUTTKh
726:R-36MUTTKh
655:R-36MUTTKh
487:1982-1988
388:R-36MUTTKh
344:Energomash
304:, burning
277:References
272:References
265:R-36MUTTKh
226:Dimensions
110:Propellant
58:Energomash
2541:Castor 30
2421:Zefiro 40
2416:Zefiro 23
2357:SpaB-140C
1754:NK-33, 44
1664:cryogenic
1510:Methalox
1329:Hydrolox
1321:Cryogenic
1062:"RD-263F"
1041:"History"
661:MR-UR-100
569:, vacuum
484:1970-1976
481:1969-1975
406:MR-UR-100
62:V.Glushko
49:1969-1975
2556:Orbus-21
2411:Zefiro 9
2174:Ukraine
1952:Aerozine
1940:Storable
1832:Ukraine
1774:RD-0110R
1671:Kerolox
1200:"RD-274"
1094:"RD-273"
982:"RD-268"
950:"RD-264"
859:"RD-263"
747:See also
687:Retired
459:RD-263F
363:Versions
247:Dry mass
239:Diameter
197:, vacuum
185:pressure
183:Chamber
54:Designer
2615:italics
2576:Star 48
2571:Star 37
2551:Orbus-6
2472:Israel
2406:Waxwing
2362:Europe
2354:SpaB-65
2256:Russia
2121:RD-0237
2116:RD-0236
2087:Russia
2066:Israel
2026:Europe
1870:Kestrel
1816:S1.5400
1779:RD-0124
1745:Russia
1738:SCE-200
1634:Europe
1627:RD-0169
1622:Russia
1548:Longyun
1541:Lingyun
1459:RD-0146
1453:RD-0120
1444:Russia
1401:Vulcain
1387:Europe
1310:Liquid
1286:orbital
701:Modules
684:Retired
678:Status
641:Unknown
603:Length
473:RD-274
445:RD-273
442:RD-268
439:RD-263
436:Engine
420:RD-263F
400:Index:
378:Index:
319:in the
297:) is a
255:Used in
154:Chamber
2531:AJ-60A
2496:KM-V2b
2487:Japan
2461:Salman
2427:India
2401:Topaze
2366:Mage 1
2331:China
2322:Solid
2229:TR-201
2193:RD-856
2188:RD-855
2178:RD-843
2168:S5.98M
2157:RD-270
2051:India
2045:Viking
2035:Astris
2030:Aestus
2020:YF-50D
1996:China
1905:RS-27A
1895:Merlin
1885:LR-105
1849:RD-810
1842:RD-801
1826:TEPREL
1822:Spain
1810:RD-193
1799:RD-180
1789:RD-120
1733:India
1726:Welkin
1719:YF-130
1713:YF-115
1708:YF-102
1703:YF-100
1687:China
1615:Aeon R
1608:Aeon 1
1595:Raptor
1579:YF-215
1572:YF-209
1565:TQ-15A
1529:China
1422:Japan
1411:CE-7.5
1407:India
1362:YF-75D
1348:China
740:R-36M2
732:RD-274
718:15D119
716:Index
710:RD-264
671:R-36M2
617:Width
595:295.6s
575:318.5s
501:using
496:Liquid
467:RD-264
456:15D168
453:15D117
424:R-36M2
416:RD-273
402:15D168
394:RD-268
380:15D117
372:RD-263
348:RD-270
333:15D119
331:Index
325:RD-264
299:liquid
295:15D117
293:Index
287:RD-263
231:Length
95:Status
18:RD-264
2596:X-254
2591:X-248
2581:UA120
2561:Orion
2536:Algol
2521:SRB-A
2516:M-34c
2491:KM-V1
2481:RSA-3
2457:Iran
2350:FG-47
2345:FG-46
2340:FG-36
2335:FG-02
2296:XLR81
2290:RS-88
2285:Curie
2275:Gamma
2250:Other
2234:XLR81
2223:RS-88
2218:LR-91
2213:LR-87
2163:S5.92
2091:17D61
2060:Vikas
2040:Vexin
2015:YF-40
2010:YF-23
1983:, or
1963:, or
1957:UH 25
1925:XLR50
1910:RS-56
1900:RS-27
1880:LR-89
1875:LR-79
1759:RD-58
1749:NK-15
1697:TH-12
1691:TH-11
1662:Semi-
1559:TQ-12
1554:TQ-11
1534:BF-20
1499:RS-68
1494:RS-25
1471:BE-3U
1416:CE-20
1396:Vinci
1380:YF-90
1373:YF-79
1367:YF-77
1357:YF-75
1352:YF-73
1179:(PDF)
793:LR-87
779:Dnepr
769:R-36M
722:R-36M
651:R-36M
598:296s
578:318s
418:(AKA
384:R-36M
357:Dnepr
337:R-36M
261:R-36M
139:Cycle
89:Dnepr
85:R-36M
2586:SRMU
2511:M-34
2506:M-24
2501:M-14
2476:LK-1
2466:Rafe
2451:S200
2446:S139
2396:P230
2391:P120
2324:fuel
2208:AJ10
2070:LK-4
1965:UDMH
1915:S-3D
1836:RD-8
1675:RP-1
1646:M-10
1590:BE-4
1489:RL10
1478:BE-7
1437:LE-9
1431:LE-7
1426:LE-5
1391:HM7B
1312:fuel
1284:for
1280:and
773:ICBM
736:GRAU
724:and
714:GRAU
647:Use
592:293s
572:318s
514:UDMH
450:AKA
398:GRAU
386:and
376:GRAU
353:ICBM
329:GRAU
317:UDMH
315:and
291:GRAU
285:The
263:and
134:2.67
125:UDMH
87:and
46:Date
40:USSR
2546:GEM
2441:S12
2386:P80
2381:PAP
2376:P-6
2371:P-4
2271:UK
2055:PS4
1985:HNO
1981:MON
1961:MMH
1865:H-1
1860:F-1
1679:LOX
1521:LOX
1484:J-2
1340:LOX
470:N/A
2633::
2436:S9
2431:S7
1979:,
1968:/
1959:,
1954:,
1677:/
1519:/
1514:CH
1338:/
1333:LH
1202:.
1149:.
1133:19
1131:.
1117:^
1096:.
1085:^
1064:.
1053:^
1019:.
1005:^
984:.
973:^
952:.
941:^
927:.
910:^
894:.
882:^
861:.
844:^
828:.
816:^
781:-
771:-
587:sp
567:sp
221:7°
123:/
80:LV
60:,
2298:*
2292:*
2236:*
2225:*
1990:)
1987:3
1976:4
1974:O
1972:2
1970:N
1950:(
1681:)
1673:(
1523:)
1516:4
1512:(
1342:)
1335:2
1331:(
1270:e
1263:t
1256:v
1217:.
1188:.
1164:.
1111:.
1079:.
1029:.
999:.
967:.
904:.
876:.
838:.
789:.
734:(
712:(
584:I
564:I
512:/
509:4
507:O
505:2
503:N
396:(
374:(
327:(
312:4
310:O
308:2
306:N
289:(
157:1
120:4
118:O
116:2
114:N
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.