2302:
744:
339:
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
2635:
2439:
2630:
2434:
913:
2625:
2429:
2424:
2419:
2043:
1257:
1219:
1135:
1029:
1288:
1227:
1050:
1188:
1082:
970:
2640:
2554:
938:
847:
694:
Some of these engines were bundled into modules of multiple engines. The relevant modules and auxiliary engines are:
2645:
487:
309:
131:
1953:
502:
305:
113:
1235:
2584:
1250:
1164:
2574:
1908:
1627:
1589:
921:
775:
757:
728:
714:
710:
659:
643:
639:
412:
376:
372:
341:
325:
253:
249:
73:
1873:
1868:
1969:
1298:
484:
92:
1863:
2310:
1536:
1529:
1389:
1243:
2394:
2263:
2033:
2023:
1714:
1696:
328:
1935:
2579:
2529:
2449:
2409:
2404:
2399:
2273:
2048:
1998:
1936:
1384:
785:
2454:
2549:
2544:
2539:
2534:
2524:
1958:
1270:
491:
294:
102:
1603:
1596:
8:
2559:
2379:
2079:
1949:
1634:
1274:
2374:
791:
287:
1005:
2504:
2484:
194:
183:
50:
1143:
1903:
1321:
1033:
205:
1058:
1878:
1858:
1853:
1848:
1472:
1309:
1277:
1265:
1196:
1090:
978:
946:
917:
855:
771:
767:
345:
332:
77:
46:
411:): Improved version based on the RD-263F upgrade project. Version used on the
2619:
1883:
1667:
1583:
1509:
1328:
1266:
653:
649:
398:
394:
290:
880:
814:
749:
1973:
1940:
2599:* Different versions of the engine use different propellant combinations
2389:
2028:
2364:
2359:
2008:
1116:
Lardier, Christian. "Liquid
Propellant Engines in the Soviet Union".
335:, instead of both stages, arguing that they were overworked with the
2469:
2464:
2384:
2369:
2354:
2058:
1762:
727:
Index ): A module comprising four RD-273. Propulsion module of the
173:
60:
2564:
2119:
2114:
2109:
2104:
2099:
2094:
2089:
2084:
1804:
1767:
1757:
1752:
1726:
1615:
1502:
1447:
1441:
1228:
Encyclopedia
Astronautica information on the propulsion module.
2519:
2253:
2248:
2217:
2186:
2181:
2176:
2171:
2166:
2156:
2145:
2134:
2129:
2124:
2068:
2018:
1893:
1837:
1830:
1814:
1798:
1792:
1787:
1782:
1777:
1772:
1707:
1701:
1691:
1567:
1560:
1399:
1350:
336:
2569:
2509:
2338:
2333:
2328:
2323:
2284:
2278:
2222:
2211:
2201:
2151:
2003:
1993:
1945:
1913:
1898:
1888:
1747:
1742:
1737:
1685:
1679:
1553:
1547:
1542:
1522:
1487:
1482:
1459:
1436:
1404:
1368:
1361:
1355:
1345:
1340:
781:
709:): A module comprising four RD-263. Propulsion module of the
2206:
2196:
1988:
1824:
1663:
1578:
1477:
1466:
1425:
1419:
1414:
1379:
761:
724:
702:
386:
364:
317:
279:
28:
2499:
2494:
2489:
2479:
784:, twin-chamber American rocket engine family used on the
739:
312:
cycle. Four RD-263 engines form a propulsion module
1659:
2636:Rocket engines using the staged combustion cycle
2617:
1111:
1109:
1107:
999:
997:
995:
764:for which this engine was originally developed.
1157:
1251:
1104:
1022:
992:
1077:
1075:
1045:
1043:
874:
872:
331:only ordered the first stage propulsion to
2631:Rocket engines using hypergolic propellant
1258:
1244:
1220:KbKhA official information on the engine.
965:
963:
933:
931:
908:
906:
904:
902:
900:
842:
840:
838:
836:
834:
808:
806:
1181:
1170:. Nuclear Threat Initiative. August 2012
1124:. American Astronautical Society: 39–73.
1072:
1040:
869:
1128:
960:
928:
897:
831:
803:
356:The basic engine has been used for the
2618:
68:
1239:
505:propellant with an O/F ratio of 2.67
1289:Comparison of orbital rocket engines
1003:
167:1,040 kilonewtons (230,000 lbf)
159:1,128 kilonewtons (254,000 lbf)
1115:
731:(15A18M) and (15A18M2) first stage.
662:(15A18M) and (15A18M2) first stage
415:(15A18M) and (15A18M2) first stage.
13:
2626:Rocket engines of the Soviet Union
14:
2657:
1213:
1118:Thirty-third IAA History Simposia
547:1,130 kN (250,000 lbf)
533:1,240 kN (280,000 lbf)
178:20.6 megapascals (2,990 psi)
2300:
1142:. Missile Threat. Archived from
1032:. NPO Energomash. Archived from
914:"NPO Energomash list of engines"
742:
544:1,130 kN (250,000 lbf)
541:1,040 kN (230,000 lbf)
530:1,240 kN (280,000 lbf)
527:1,130 kN (250,000 lbf)
878:
815:"R-36M/15A14/SS-18/Satan/RS-20"
812:
792:Rocket engine using liquid fuel
519:22.6 MPa (3,280 psi)
488:oxidizer rich staged combustion
371:): Initial version used on the
348:remain operational as of 2015.
310:oxidizer rich staged combustion
132:Oxidizer-rich staged combustion
717:first stage (15А14 and 15A18).
516:22.6 MPa (3,280 psi)
513:20.6 MPa (2,990 psi)
379:first stage (15А14 and 15A18).
231:1,080 millimetres (43 in)
223:2,150 millimetres (85 in)
1:
2085:RD-0202 to 0206, 0208 to 0213
797:
239:870 kilograms (1,920 lb)
612:1,083 mm (42.6 in)
510:Combustion chamber pressure
256:core stage (15А14 and 15A18)
7:
735:
626:770 kg (1,700 lb)
623:870 kg (1,920 lb)
615:1,080 mm (43 in)
601:2,150 mm (85 in)
351:
200:293 s (2.87 km/s)
189:318 s (3.12 km/s)
10:
2662:
689:
609:1,080 mm (43 in)
598:2,150 mm (85 in)
595:2,150 mm (85 in)
420:RD-0210 family of engines
2641:Energomash rocket engines
2595:
2309:
2298:
2238:
1928:
1650:
1498:
1317:
1308:
1297:
1284:
1193:Encyclopedia Astronautica
1087:Encyclopedia Astronautica
1055:Encyclopedia Astronautica
975:Encyclopedia Astronautica
943:Encyclopedia Astronautica
852:Encyclopedia Astronautica
683:
483:
393:): Variation used on the
265:
260:
248:
243:
235:
227:
219:
214:
204:
193:
182:
171:
163:
155:
150:
142:
137:
127:
119:
98:
91:
83:
66:
56:
42:
34:
24:
2646:Yuzhmash rocket engines
2130:RD-250 to 252, 261, 262
1010:Jonathan's Space Report
788:of US launch vehicles.
2606:are under development
1994:YF-20, 21, 22, 24, 25
1773:RD-107, 108, 117, 118
1165:"Kazakhstan Missiles"
774:that is a repurposed
1136:"Ballistic Missiles"
1004:McDowell, Jonathan.
881:"The Dnepr launcher"
401:(15A16) first stage.
2095:RD-0216, 0217, 0235
1758:RD-0107, 0108, 0110
924:on 7 November 2014.
885:RussianSpaceWeb.com
858:on January 13, 2003
819:RussianSpaceWeb.com
656:(15A16) first stage
421:
21:
646:(15A18) core stage
538:Thrust, sea level
453:Propulsion module
419:
93:Liquid-fuel engine
19:
2613:
2612:
2555:Space Shuttle SRB
2296:
2295:
2234:
2233:
1924:
1923:
1646:
1645:
1140:missilethreat.com
1036:on 21 March 2016.
1006:"Russian engines"
687:
686:
670:Out of production
272:
271:
164:Thrust, sea-level
87:Out of production
25:Country of origin
2653:
2304:
2303:
2140:RD-263, 268, 273
2071:along other LREs
1933:
1932:
1793:RD-191, 151, 181
1657:
1656:
1315:
1314:
1306:
1305:
1260:
1253:
1246:
1237:
1236:
1208:
1207:
1205:
1204:
1195:. Archived from
1185:
1179:
1178:
1176:
1175:
1169:
1161:
1155:
1154:
1152:
1151:
1132:
1126:
1125:
1113:
1102:
1101:
1099:
1098:
1089:. Archived from
1079:
1070:
1069:
1067:
1066:
1057:. Archived from
1047:
1038:
1037:
1026:
1020:
1019:
1017:
1016:
1001:
990:
989:
987:
986:
977:. Archived from
967:
958:
957:
955:
954:
945:. Archived from
935:
926:
925:
920:. Archived from
910:
895:
894:
892:
891:
876:
867:
866:
864:
863:
854:. Archived from
844:
829:
828:
826:
825:
810:
752:
747:
746:
745:
422:
418:
195:Specific impulse
184:Specific impulse
70:
22:
20:RD-263 (РД-263)
18:
2661:
2660:
2656:
2655:
2654:
2652:
2651:
2650:
2616:
2615:
2614:
2609:
2591:
2312:
2305:
2301:
2292:
2230:
2120:RD-0255 to 0257
2115:RD-0243 to 0245
1977:
1966:
1962:
1956:
1944:
1920:
1661:
1652:
1642:
1506:
1500:
1494:
1325:
1319:
1300:
1293:
1280:
1278:launch vehicles
1264:
1216:
1211:
1202:
1200:
1187:
1186:
1182:
1173:
1171:
1167:
1163:
1162:
1158:
1149:
1147:
1134:
1133:
1129:
1114:
1105:
1096:
1094:
1081:
1080:
1073:
1064:
1062:
1061:on May 31, 2002
1049:
1048:
1041:
1028:
1027:
1023:
1014:
1012:
1002:
993:
984:
982:
969:
968:
961:
952:
950:
937:
936:
929:
912:
911:
898:
889:
887:
877:
870:
861:
859:
846:
845:
832:
823:
821:
811:
804:
800:
748:
743:
741:
738:
692:
577:
557:
524:Thrust, vacuum
499:
495:
354:
344:as well as the
302:
298:
110:
106:
17:
12:
11:
5:
2659:
2649:
2648:
2643:
2638:
2633:
2628:
2611:
2610:
2608:
2607:
2600:
2596:
2593:
2592:
2590:
2589:
2588:
2587:
2582:
2577:
2572:
2567:
2562:
2557:
2552:
2547:
2542:
2537:
2532:
2527:
2522:
2516:United States
2514:
2513:
2512:
2507:
2502:
2497:
2492:
2487:
2482:
2474:
2473:
2472:
2467:
2459:
2458:
2457:
2452:
2444:
2443:
2442:
2437:
2432:
2427:
2422:
2414:
2413:
2412:
2407:
2402:
2397:
2392:
2387:
2382:
2377:
2372:
2367:
2362:
2357:
2349:
2348:
2347:
2344:
2341:
2336:
2331:
2326:
2317:
2315:
2307:
2306:
2299:
2297:
2294:
2293:
2291:
2290:
2289:
2288:
2282:
2276:
2270:United States
2268:
2267:
2266:
2258:
2257:
2256:
2251:
2242:
2240:
2236:
2235:
2232:
2231:
2229:
2228:
2227:
2226:
2220:
2215:
2209:
2204:
2199:
2193:United States
2191:
2190:
2189:
2184:
2179:
2174:
2169:
2161:
2160:
2159:
2154:
2149:
2142:
2137:
2132:
2127:
2122:
2117:
2112:
2107:
2102:
2097:
2092:
2087:
2082:
2074:
2073:
2072:
2063:
2062:
2061:
2053:
2052:
2051:
2046:
2038:
2037:
2036:
2031:
2026:
2021:
2013:
2012:
2011:
2006:
2001:
1996:
1991:
1982:
1980:
1975:
1964:
1960:
1930:
1926:
1925:
1922:
1921:
1919:
1918:
1917:
1916:
1911:
1906:
1901:
1896:
1891:
1886:
1881:
1879:LR70-NA , S-3D
1876:
1871:
1866:
1861:
1856:
1851:
1845:United States
1843:
1842:
1841:
1834:
1827:
1819:
1818:
1817:
1809:
1808:
1807:
1802:
1795:
1790:
1785:
1780:
1775:
1770:
1765:
1760:
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1750:
1745:
1740:
1732:
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1730:
1720:
1719:
1718:
1711:
1704:
1699:
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1682:
1673:
1671:
1654:
1648:
1647:
1644:
1643:
1641:
1640:
1639:
1638:
1631:
1621:
1620:
1619:
1609:
1608:
1607:
1600:
1593:
1586:
1581:
1575:United States
1573:
1572:
1571:
1564:
1557:
1550:
1545:
1540:
1533:
1526:
1515:
1513:
1504:
1496:
1495:
1493:
1492:
1491:
1490:
1485:
1480:
1475:
1470:
1463:
1455:United States
1453:
1452:
1451:
1444:
1439:
1431:
1430:
1429:
1422:
1417:
1409:
1408:
1407:
1402:
1394:
1393:
1392:
1387:
1382:
1374:
1373:
1372:
1365:
1358:
1353:
1348:
1343:
1334:
1332:
1323:
1312:
1303:
1295:
1294:
1292:
1291:
1285:
1282:
1281:
1267:Rocket engines
1263:
1262:
1255:
1248:
1240:
1234:
1233:
1225:
1215:
1214:External links
1212:
1210:
1209:
1199:on May 6, 2002
1180:
1156:
1127:
1103:
1093:on May 6, 2002
1071:
1039:
1021:
991:
959:
927:
918:NPO Energomash
896:
879:Zak, Anatoly.
868:
830:
813:Zak, Anatoly.
801:
799:
796:
795:
794:
789:
779:
772:launch vehicle
765:
754:
753:
737:
734:
733:
732:
718:
691:
688:
685:
684:
682:
678:
677:
674:
671:
668:
664:
663:
657:
654:MR-UR-100UTTKh
647:
637:
633:
632:
627:
624:
621:
617:
616:
613:
610:
607:
603:
602:
599:
596:
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582:
579:
575:
569:
568:
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562:
559:
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549:
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542:
539:
535:
534:
531:
528:
525:
521:
520:
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514:
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493:
482:
478:
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468:
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457:
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450:
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446:
443:
440:
436:
435:
432:
429:
426:
417:
416:
402:
399:MR-UR-100UTTKh
380:
353:
350:
300:
296:
270:
269:
267:
263:
262:
258:
257:
246:
245:
241:
240:
237:
233:
232:
229:
225:
224:
221:
217:
216:
212:
211:
208:
202:
201:
198:
191:
190:
187:
180:
179:
176:
169:
168:
165:
161:
160:
157:
156:Thrust, vacuum
153:
152:
148:
147:
144:
140:
139:
135:
134:
129:
125:
124:
121:
117:
116:
108:
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100:
96:
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81:
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71:
64:
63:
58:
54:
53:
44:
40:
39:
36:
32:
31:
26:
15:
9:
6:
4:
3:
2:
2658:
2647:
2644:
2642:
2639:
2637:
2634:
2632:
2629:
2627:
2624:
2623:
2621:
2605:
2601:
2598:
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2526:
2523:
2521:
2518:
2517:
2515:
2511:
2508:
2506:
2503:
2501:
2498:
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2332:
2330:
2327:
2325:
2322:
2321:
2319:
2318:
2316:
2314:
2308:
2286:
2283:
2280:
2277:
2275:
2272:
2271:
2269:
2265:
2262:
2261:
2259:
2255:
2254:RD-211 to 214
2252:
2250:
2247:
2246:
2244:
2243:
2241:
2237:
2224:
2221:
2219:
2216:
2213:
2210:
2208:
2205:
2203:
2200:
2198:
2195:
2194:
2192:
2188:
2185:
2183:
2180:
2178:
2175:
2173:
2170:
2168:
2165:
2164:
2162:
2158:
2155:
2153:
2150:
2148:
2147:
2143:
2141:
2138:
2136:
2133:
2131:
2128:
2126:
2125:RD-215 to 219
2123:
2121:
2118:
2116:
2113:
2111:
2108:
2106:
2103:
2101:
2100:RD-0233, 0234
2098:
2096:
2093:
2091:
2090:RD-0207, 0214
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291:rocket engine
289:
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138:Configuration
136:
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120:Mixture ratio
118:
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37:
33:
30:
27:
23:
16:Rocket engine
2603:
2144:
2139:
2065:North Korea
1836:
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1797:
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1465:
1458:
1446:
1424:
1367:
1360:
1271:solid motors
1229:
1221:
1201:. Retrieved
1197:the original
1192:
1183:
1172:. Retrieved
1159:
1148:. Retrieved
1144:the original
1139:
1130:
1121:
1117:
1095:. Retrieved
1091:the original
1086:
1063:. Retrieved
1059:the original
1054:
1034:the original
1024:
1013:. Retrieved
1009:
983:. Retrieved
979:the original
974:
951:. Retrieved
947:the original
942:
922:the original
888:. Retrieved
884:
860:. Retrieved
856:the original
851:
822:. Retrieved
818:
786:Titan series
750:Space portal
720:
706:
698:
693:
652:(15А15) and
642:(15А14) and
629:
578:, sea level
572:
552:
481:Engine type
467:Development
408:
404:
397:(15А15) and
390:
382:
368:
360:
355:
321:
313:
283:
275:
273:
206:Gimbal range
57:Manufacturer
2602:Engines in
2249:RD-109, 119
2187:RD-864, 869
2172:RD-854, 861
2135:RD-253, 275
1783:RD-170, 171
681:References
620:Dry weight
329:KB Yuzhnoye
324:). For the
197:, sea-level
151:Performance
67:Associated
61:PA Yuzhmash
2620:Categories
1989:YF-1, 2, 3
1937:Hypergolic
1909:Rutherford
1628:Prometheus
1590:Archimedes
1230:(Archived)
1222:(Archived)
1203:2015-07-24
1174:2015-07-24
1150:2015-07-24
1097:2015-07-24
1065:2015-07-24
1015:2015-07-24
985:2015-07-24
953:2015-06-20
890:2015-06-20
862:2015-06-20
824:2015-06-20
798:References
776:R-36MUTTKh
715:R-36MUTTKh
644:R-36MUTTKh
476:1982-1988
377:R-36MUTTKh
333:Energomash
293:, burning
266:References
261:References
254:R-36MUTTKh
215:Dimensions
99:Propellant
47:Energomash
2530:Castor 30
2410:Zefiro 40
2405:Zefiro 23
2346:SpaB-140C
1743:NK-33, 44
1653:cryogenic
1499:Methalox
1318:Hydrolox
1310:Cryogenic
1051:"RD-263F"
1030:"History"
650:MR-UR-100
558:, vacuum
473:1970-1976
470:1969-1975
395:MR-UR-100
51:V.Glushko
38:1969-1975
2545:Orbus-21
2400:Zefiro 9
2163:Ukraine
1941:Aerozine
1929:Storable
1821:Ukraine
1763:RD-0110R
1660:Kerolox
1189:"RD-274"
1083:"RD-273"
971:"RD-268"
939:"RD-264"
848:"RD-263"
736:See also
676:Retired
448:RD-263F
352:Versions
236:Dry mass
228:Diameter
186:, vacuum
174:pressure
172:Chamber
43:Designer
2604:italics
2565:Star 48
2560:Star 37
2540:Orbus-6
2461:Israel
2395:Waxwing
2351:Europe
2343:SpaB-65
2245:Russia
2110:RD-0237
2105:RD-0236
2076:Russia
2055:Israel
2015:Europe
1859:Kestrel
1805:S1.5400
1768:RD-0124
1734:Russia
1727:SCE-200
1623:Europe
1616:RD-0169
1611:Russia
1537:Longyun
1530:Lingyun
1448:RD-0146
1442:RD-0120
1433:Russia
1390:Vulcain
1376:Europe
1299:Liquid
1275:orbital
690:Modules
673:Retired
667:Status
630:Unknown
592:Length
462:RD-274
434:RD-273
431:RD-268
428:RD-263
425:Engine
409:RD-263F
389:Index:
367:Index:
308:in the
286:) is a
244:Used in
143:Chamber
2520:AJ-60A
2485:KM-V2b
2476:Japan
2450:Salman
2416:India
2390:Topaze
2355:Mage 1
2320:China
2311:Solid
2218:TR-201
2182:RD-856
2177:RD-855
2167:RD-843
2157:S5.98M
2146:RD-270
2040:India
2034:Viking
2024:Astris
2019:Aestus
2009:YF-50D
1985:China
1894:RS-27A
1884:Merlin
1874:LR-105
1838:RD-810
1831:RD-801
1815:TEPREL
1811:Spain
1799:RD-193
1788:RD-180
1778:RD-120
1722:India
1715:Welkin
1708:YF-130
1702:YF-115
1697:YF-102
1692:YF-100
1676:China
1604:Aeon R
1597:Aeon 1
1584:Raptor
1568:YF-215
1561:YF-209
1554:TQ-15A
1518:China
1411:Japan
1400:CE-7.5
1396:India
1351:YF-75D
1337:China
729:R-36M2
721:RD-274
707:15D119
705:Index
699:RD-264
660:R-36M2
606:Width
584:295.6s
564:318.5s
490:using
485:Liquid
456:RD-264
445:15D168
442:15D117
413:R-36M2
405:RD-273
391:15D168
383:RD-268
369:15D117
361:RD-263
337:RD-270
322:15D119
320:Index
314:RD-264
288:liquid
284:15D117
282:Index
276:RD-263
220:Length
84:Status
2585:X-254
2580:X-248
2570:UA120
2550:Orion
2525:Algol
2510:SRB-A
2505:M-34c
2480:KM-V1
2470:RSA-3
2446:Iran
2339:FG-47
2334:FG-46
2329:FG-36
2324:FG-02
2285:XLR81
2279:RS-88
2274:Curie
2264:Gamma
2239:Other
2223:XLR81
2212:RS-88
2207:LR-91
2202:LR-87
2152:S5.92
2080:17D61
2049:Vikas
2029:Vexin
2004:YF-40
1999:YF-23
1972:, or
1952:, or
1946:UH 25
1914:XLR50
1899:RS-56
1889:RS-27
1869:LR-89
1864:LR-79
1748:RD-58
1738:NK-15
1686:TH-12
1680:TH-11
1651:Semi-
1548:TQ-12
1543:TQ-11
1523:BF-20
1488:RS-68
1483:RS-25
1460:BE-3U
1405:CE-20
1385:Vinci
1369:YF-90
1362:YF-79
1356:YF-77
1346:YF-75
1341:YF-73
1168:(PDF)
782:LR-87
768:Dnepr
758:R-36M
711:R-36M
640:R-36M
587:296s
567:318s
407:(AKA
373:R-36M
346:Dnepr
326:R-36M
250:R-36M
128:Cycle
78:Dnepr
74:R-36M
2575:SRMU
2500:M-34
2495:M-24
2490:M-14
2465:LK-1
2455:Rafe
2440:S200
2435:S139
2385:P230
2380:P120
2313:fuel
2197:AJ10
2059:LK-4
1954:UDMH
1904:S-3D
1825:RD-8
1664:RP-1
1635:M-10
1579:BE-4
1478:RL10
1467:BE-7
1426:LE-9
1420:LE-7
1415:LE-5
1380:HM7B
1301:fuel
1273:for
1269:and
762:ICBM
725:GRAU
713:and
703:GRAU
636:Use
581:293s
561:318s
503:UDMH
439:AKA
387:GRAU
375:and
365:GRAU
342:ICBM
318:GRAU
306:UDMH
304:and
280:GRAU
274:The
252:and
123:2.67
114:UDMH
76:and
35:Date
29:USSR
2535:GEM
2430:S12
2375:P80
2370:PAP
2365:P-6
2360:P-4
2260:UK
2044:PS4
1974:HNO
1970:MON
1950:MMH
1854:H-1
1849:F-1
1668:LOX
1510:LOX
1473:J-2
1329:LOX
459:N/A
2622::
2425:S9
2420:S7
1968:,
1957:/
1948:,
1943:,
1666:/
1508:/
1503:CH
1327:/
1322:LH
1191:.
1138:.
1122:19
1120:.
1106:^
1085:.
1074:^
1053:.
1042:^
1008:.
994:^
973:.
962:^
941:.
930:^
916:.
899:^
883:.
871:^
850:.
833:^
817:.
805:^
770:-
760:-
576:sp
556:sp
210:7°
112:/
69:LV
49:,
2287:*
2281:*
2225:*
2214:*
1979:)
1976:3
1965:4
1963:O
1961:2
1959:N
1939:(
1670:)
1662:(
1512:)
1505:4
1501:(
1331:)
1324:2
1320:(
1259:e
1252:t
1245:v
1206:.
1177:.
1153:.
1100:.
1068:.
1018:.
988:.
956:.
893:.
865:.
827:.
778:.
723:(
701:(
573:I
553:I
501:/
498:4
496:O
494:2
492:N
385:(
363:(
316:(
301:4
299:O
297:2
295:N
278:(
146:1
109:4
107:O
105:2
103:N
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.