415:
suction performance, the RD-0110 turbopump has a dual inlet design with back to back centrifugal impellers. This allows it to work at relatively low inlet pressures without requiring additional booster pumps. The turbine is driven by a fuel rich gas generator. The ignition system for both the gas generator and the combustion chamber is done by pyrotechnic devices. The engine control is handled by a regulator, a throttle and a set of valves. It can throttle between 100% and 90.5%, with the option of 107% for a short time in emergencies.
1998:
38:
419:
instabilities at start up were still observed. Even though the start instabilities were relatively rare at 1 in 60 to 80, and only on acceptance bench, great effort was made to eliminate the issue. Thanks to acoustic studies and modelling, a solution was found. Six combustible longitudinal felt ribs were placed at the inner surface of the combustion chamber and this solved the issue permanently.
394:. A particular problem observed during acceptance testing were high frequency instabilities, particularly during the start sequence. But it was solved by installing of longitudinal felt ribs on the combustion chamber. The development of the RD-0110 was performed in 9 months during 1963, with its inaugural flight happening in 1964. It is also used on the
427:
corrugated jacket to save weight. All these sections use steel for construction. Given the extreme temperatures at the throat section, this part is made of copper alloy with milled channels and an external lining. A separate film cooling system is implemented though a different manifold and is injected though a circular slot upstream of the throat.
414:
The RD-0110 was created in a period when KBKhA had just started to design rocket engines. After many studies, simplicity and reliability were the main drivers of the design. For this reason a single shaft integrating the LOX pump, the RG-1 pump and the turbine was chosen. To provide acceptable
426:
system. As most other Soviet designs, it uses a corrugated metal construction for the cooling jackets. The thrust chamber and upper nozzle sections has the corrugated metal sandwiched between an inner and outer metal layers. The lower section of the nozzle has no external lining, exposing the
418:
During development, combustion instability issues were observed. The problem was found to be intimately related to the injection system design. It was finally solved by developing an optimized bi-propellant centrifugal atomizer design. During certification testing, high frequency combustion
382:
kept the same characteristics and performance of the RD-0107 while fully complying with the crew rating regulations. This engine had its first flight on
November 16, 1963, and last flew on June 29, 1976.
378:
Block-I, a version of the engine that complied with the human rating 3K Regulations was needed. During 1963 OKB-154 developed this new version of the engine. Known with by the GRAU index 8D715P, the
2336:
2331:
2135:
2326:
953:
2130:
912:
550:
634:
984:
390:
Block-I, OKB-154 did an improvement program that put special emphasis on the reliability of the engine. This project gave birth to the
2250:
886:
325:
of the stage. It has an extensive flight history with its initial versions having flown more than 57 years ago (as of
February 2018).
2321:
1649:
2125:
2120:
2115:
1739:
786:
663:
926:
761:
575:
2341:
423:
716:
406:. It has flown over 1350 times, and accumulated more than 336,500 s of burn time and is still flown many times per year.
946:
321:. It has four fixed nozzles and the output of the gas generator is directed to four secondary vernier nozzles to supply
318:
158:
371:
development. The engine had its debut flight on
October 10, 1960, and the last Molniya flight was on October 22, 1967.
2270:
1604:
1323:
1285:
837:
521:
76:
607:
Rubinsky, Vitaly R. (1995). "Chapter 4: Combustion
Instability in the RD-0110 Engine". In Anderson, William E.;
1665:
994:
126:
931:
2006:
1232:
1225:
1085:
939:
2090:
1959:
1729:
1719:
1410:
1392:
688:
360:
191:
2280:
2275:
2225:
2145:
2105:
2100:
2095:
1969:
1744:
1694:
1632:
1080:
509:
395:
269:
101:
2245:
2240:
2235:
2230:
2220:
1654:
966:
443:
Modifications to the RD-0107 design have led to production of three distinct versions of the engine:
2255:
2075:
1775:
1645:
1330:
970:
909:
554:
2070:
614:
Progress in
Astronautics and Aeronautics Volume 169: Liquid Rocket Engine Combustion Instability
608:
852:
2150:
882:
812:
630:
140:
2200:
2180:
1299:
1292:
622:
490:
459:
403:
375:
212:
1599:
1017:
916:
664:"RD0107, RD0108, RD0110. Molniya (8K78), Voskhod (8K78M), Soyuz (11A511У) launch vehicles"
1574:
1554:
1549:
1544:
1168:
1005:
973:
470:
337:
322:
37:
2315:
1579:
1363:
1279:
1205:
1024:
962:
310:
306:
359:, also designed by OKB-154. It also leveraged the experience in the field from the
790:
667:
1669:
1636:
1569:
1564:
1559:
765:
612:
579:
451:
Index: 8D715K), also known as RD-461 or RO-8. Used on unmanned
Voskhod boosters.
720:
353:
740:
435:
The RD-0107/0108/0110 engines are produced in the
Voronezh Mechanical Plant.
1704:
503:
458:
Index: 8D715P), also known as 11D55, RD-461 or RO-8. Used on the two manned
387:
341:
265:
97:
787:"RD0105. Luna (8K72) launch vehicle. RD0109. Vostok (8K72K) launch vehicle"
2165:
2160:
2080:
2065:
2050:
1754:
1458:
689:"Turbopumps for Gas Generator and Staged Combustion Cycle Rocket Engines"
527:
486:
482:
314:
202:
2295:* Different versions of the engine use different propellant combinations
2260:
2085:
2060:
2055:
1815:
1810:
1805:
1800:
1795:
1790:
1785:
1780:
1724:
1500:
1463:
1448:
1422:
1311:
1198:
1143:
1137:
478:
474:
399:
368:
364:
333:
111:
17:
524:– A space hardware manufacturer company that manufactures the RD-0110.
2215:
1949:
1944:
1913:
1882:
1877:
1872:
1867:
1862:
1852:
1841:
1835:
1830:
1825:
1820:
1764:
1714:
1589:
1533:
1526:
1510:
1494:
1488:
1483:
1478:
1473:
1468:
1403:
1397:
1387:
1263:
1256:
1095:
1046:
626:
833:
2265:
2205:
2034:
2029:
2024:
2019:
1980:
1974:
1918:
1907:
1897:
1847:
1699:
1689:
1641:
1609:
1594:
1584:
1443:
1438:
1433:
1381:
1375:
1249:
1243:
1238:
1218:
1183:
1178:
1155:
1132:
1100:
1064:
1057:
1051:
1041:
1036:
515:
66:
1902:
1892:
1684:
1520:
1359:
1274:
1173:
1162:
1121:
1115:
1110:
1075:
878:
695:
618:
466:
455:
448:
356:
349:
348:
was developed in the 1960 to 1961 period, based on the RD-0106 (
48:
935:
2195:
2190:
2185:
2175:
136:
469:
Index: 8D715P), also known as 11D55 or RD-461. Used on the
921:
904:
834:"Part 9: Launchers for an Early Circumlunar Programme"
340:
was tasked with developing an engine for the unmanned
530:- version of the engine modified for first stage use
2005:
1934:
1631:
1624:
1355:
1346:
1194:
1013:
1004:
993:
280:
275:
259:
251:
243:
235:
230:
222:
211:
200:
190:
182:
177:
169:
164:
154:
146:
132:
125:
117:
107:
90:
82:
72:
62:
54:
44:
683:
681:
679:
677:
602:
600:
598:
596:
658:
656:
654:
652:
462:launches and the first six Molniya-M boosters.
947:
8:
2337:Rocket engines using the gas-generator cycle
734:
732:
730:
30:
875:History of Liquid Propellant Rocket Engines
764:. Encyclopedia Astronautica. Archived from
578:. Encyclopedia Astronautica. Archived from
570:
568:
566:
564:
553:. Voronezh Mechanical Plant. Archived from
1628:
1352:
1010:
1001:
954:
940:
932:
36:
545:
543:
422:The RD-0110 uses fuel as coolant for the
2332:Rocket engines using kerosene propellant
927:РД-0110 в энциклопедии Astronautix.com.
840:from the original on 25 September 2011.
539:
352:Index: 8D715) engine that powered the
92:
29:
873:Sutton, George Paul (November 2005).
719:. Space Launch Report. Archived from
7:
985:Comparison of orbital rocket engines
398:third stage in all models until the
27:Soviet (later Russian) rocket engine
2327:Rocket engines of the Soviet Union
506:– The first LV to use the RD-0110.
25:
186:298 kilonewtons (67,000 lbf)
1996:
239:1,575 millimetres (62.0 in)
853:"Liste des lancements Voskhod"
518:– The RD-0110 designer bureau.
319:gas generator combustion cycle
247:2,240 millimetres (88 in)
207:6.8 megapascals (990 psi)
1:
1781:RD-0202 to 0206, 0208 to 0213
855:(in French). Kosmonavtika.com
815:(in French). Kosmonavtika.com
813:"Liste des lancements Molnia"
255:408.5 kilograms (901 lb)
2358:
493:and almost all Molniya-Ms.
2291:
1994:
980:
910:Voronezh Mechanical Plant
522:Voronezh Mechanical Plant
344:Block-I stage. Thus, the
264:
77:Voronezh Mechanical Plant
35:
2322:Rocket engines of Russia
374:For the crewed carrying
1826:RD-250 to 252, 261, 262
789:. KBKhA. Archived from
666:. KBKhA. Archived from
922:RSC Progress Home Page
717:"R-7/Soyuz Data Sheet"
551:"Liquid Rocket Engine"
192:Thrust-to-weight ratio
2302:are under development
1690:YF-20, 21, 22, 24, 25
1469:RD-107, 108, 117, 118
743:. russianspaceweb.com
2342:KBKhA rocket engines
881:. pp. 637–638.
512:– The most flown LV.
424:regenerative cooling
1791:RD-0216, 0217, 0235
1454:RD-0107, 0108, 0110
793:on 23 November 2011
670:on 14 October 2011.
621:. pp. 89–112.
510:Soyuz rocket family
32:
915:2021-03-06 at the
127:Liquid-fuel engine
2309:
2308:
2251:Space Shuttle SRB
1992:
1991:
1930:
1929:
1620:
1619:
1342:
1341:
851:Pillet, Nicolas.
811:Pillet, Nicolas.
768:on March 20, 2002
723:on 6 August 2010.
636:978-1-56347-183-4
582:on March 21, 2002
287:
286:
266:Molniya-M Block-I
45:Country of origin
16:(Redirected from
2349:
2000:
1999:
1836:RD-263, 268, 273
1767:along other LREs
1629:
1489:RD-191, 151, 181
1353:
1011:
1002:
956:
949:
942:
933:
893:
892:
870:
864:
863:
861:
860:
848:
842:
841:
836:. Cosmopark.ru.
830:
824:
823:
821:
820:
808:
802:
801:
799:
798:
783:
777:
776:
774:
773:
758:
752:
751:
749:
748:
736:
725:
724:
713:
707:
706:
704:
703:
693:
685:
672:
671:
660:
647:
646:
644:
643:
627:10.2514/4.866371
604:
591:
590:
588:
587:
572:
559:
558:
547:
213:Specific impulse
94:
40:
33:
21:
2357:
2356:
2352:
2351:
2350:
2348:
2347:
2346:
2312:
2311:
2310:
2305:
2287:
2008:
2001:
1997:
1988:
1926:
1816:RD-0255 to 0257
1811:RD-0243 to 0245
1673:
1662:
1658:
1652:
1640:
1616:
1357:
1348:
1338:
1202:
1196:
1190:
1021:
1015:
996:
989:
976:
974:launch vehicles
960:
917:Wayback Machine
905:KbKhA Home Page
901:
896:
889:
872:
871:
867:
858:
856:
850:
849:
845:
832:
831:
827:
818:
816:
810:
809:
805:
796:
794:
785:
784:
780:
771:
769:
760:
759:
755:
746:
744:
738:
737:
728:
715:
714:
710:
701:
699:
691:
687:
686:
675:
662:
661:
650:
641:
639:
637:
606:
605:
594:
585:
583:
574:
573:
562:
557:on 30 May 2015.
549:
548:
541:
537:
500:
441:
433:
412:
331:
28:
23:
22:
15:
12:
11:
5:
2355:
2353:
2345:
2344:
2339:
2334:
2329:
2324:
2314:
2313:
2307:
2306:
2304:
2303:
2296:
2292:
2289:
2288:
2286:
2285:
2284:
2283:
2278:
2273:
2268:
2263:
2258:
2253:
2248:
2243:
2238:
2233:
2228:
2223:
2218:
2212:United States
2210:
2209:
2208:
2203:
2198:
2193:
2188:
2183:
2178:
2170:
2169:
2168:
2163:
2155:
2154:
2153:
2148:
2140:
2139:
2138:
2133:
2128:
2123:
2118:
2110:
2109:
2108:
2103:
2098:
2093:
2088:
2083:
2078:
2073:
2068:
2063:
2058:
2053:
2045:
2044:
2043:
2040:
2037:
2032:
2027:
2022:
2013:
2011:
2003:
2002:
1995:
1993:
1990:
1989:
1987:
1986:
1985:
1984:
1978:
1972:
1966:United States
1964:
1963:
1962:
1954:
1953:
1952:
1947:
1938:
1936:
1932:
1931:
1928:
1927:
1925:
1924:
1923:
1922:
1916:
1911:
1905:
1900:
1895:
1889:United States
1887:
1886:
1885:
1880:
1875:
1870:
1865:
1857:
1856:
1855:
1850:
1845:
1838:
1833:
1828:
1823:
1818:
1813:
1808:
1803:
1798:
1793:
1788:
1783:
1778:
1770:
1769:
1768:
1759:
1758:
1757:
1749:
1748:
1747:
1742:
1734:
1733:
1732:
1727:
1722:
1717:
1709:
1708:
1707:
1702:
1697:
1692:
1687:
1678:
1676:
1671:
1660:
1656:
1626:
1622:
1621:
1618:
1617:
1615:
1614:
1613:
1612:
1607:
1602:
1597:
1592:
1587:
1582:
1577:
1575:LR70-NA , S-3D
1572:
1567:
1562:
1557:
1552:
1547:
1541:United States
1539:
1538:
1537:
1530:
1523:
1515:
1514:
1513:
1505:
1504:
1503:
1498:
1491:
1486:
1481:
1476:
1471:
1466:
1461:
1456:
1451:
1446:
1441:
1436:
1428:
1427:
1426:
1416:
1415:
1414:
1407:
1400:
1395:
1390:
1385:
1378:
1369:
1367:
1350:
1344:
1343:
1340:
1339:
1337:
1336:
1335:
1334:
1327:
1317:
1316:
1315:
1305:
1304:
1303:
1296:
1289:
1282:
1277:
1271:United States
1269:
1268:
1267:
1260:
1253:
1246:
1241:
1236:
1229:
1222:
1211:
1209:
1200:
1192:
1191:
1189:
1188:
1187:
1186:
1181:
1176:
1171:
1166:
1159:
1151:United States
1149:
1148:
1147:
1140:
1135:
1127:
1126:
1125:
1118:
1113:
1105:
1104:
1103:
1098:
1090:
1089:
1088:
1083:
1078:
1070:
1069:
1068:
1061:
1054:
1049:
1044:
1039:
1030:
1028:
1019:
1008:
999:
991:
990:
988:
987:
981:
978:
977:
963:Rocket engines
961:
959:
958:
951:
944:
936:
930:
929:
924:
919:
907:
900:
899:External links
897:
895:
894:
888:978-1563476495
887:
865:
843:
825:
803:
778:
753:
739:Zak, Anatoly.
726:
708:
673:
648:
635:
592:
560:
538:
536:
533:
532:
531:
525:
519:
513:
507:
499:
496:
495:
494:
463:
452:
440:
437:
432:
429:
411:
408:
330:
327:
323:vector control
285:
284:
282:
278:
277:
273:
272:
262:
261:
257:
256:
253:
249:
248:
245:
241:
240:
237:
233:
232:
228:
227:
224:
220:
219:
216:
209:
208:
205:
198:
197:
194:
188:
187:
184:
183:Thrust, vacuum
180:
179:
175:
174:
171:
167:
166:
162:
161:
156:
152:
151:
148:
144:
143:
134:
130:
129:
123:
122:
119:
115:
114:
109:
105:
104:
95:
88:
87:
84:
80:
79:
74:
70:
69:
64:
60:
59:
56:
52:
51:
46:
42:
41:
26:
24:
14:
13:
10:
9:
6:
4:
3:
2:
2354:
2343:
2340:
2338:
2335:
2333:
2330:
2328:
2325:
2323:
2320:
2319:
2317:
2301:
2297:
2294:
2293:
2290:
2282:
2279:
2277:
2274:
2272:
2269:
2267:
2264:
2262:
2259:
2257:
2254:
2252:
2249:
2247:
2244:
2242:
2239:
2237:
2234:
2232:
2229:
2227:
2224:
2222:
2219:
2217:
2214:
2213:
2211:
2207:
2204:
2202:
2199:
2197:
2194:
2192:
2189:
2187:
2184:
2182:
2179:
2177:
2174:
2173:
2171:
2167:
2164:
2162:
2159:
2158:
2156:
2152:
2149:
2147:
2144:
2143:
2141:
2137:
2134:
2132:
2129:
2127:
2124:
2122:
2119:
2117:
2114:
2113:
2111:
2107:
2104:
2102:
2099:
2097:
2094:
2092:
2089:
2087:
2084:
2082:
2079:
2077:
2074:
2072:
2069:
2067:
2064:
2062:
2059:
2057:
2054:
2052:
2049:
2048:
2046:
2041:
2038:
2036:
2033:
2031:
2028:
2026:
2023:
2021:
2018:
2017:
2015:
2014:
2012:
2010:
2004:
1982:
1979:
1976:
1973:
1971:
1968:
1967:
1965:
1961:
1958:
1957:
1955:
1951:
1950:RD-211 to 214
1948:
1946:
1943:
1942:
1940:
1939:
1937:
1933:
1920:
1917:
1915:
1912:
1909:
1906:
1904:
1901:
1899:
1896:
1894:
1891:
1890:
1888:
1884:
1881:
1879:
1876:
1874:
1871:
1869:
1866:
1864:
1861:
1860:
1858:
1854:
1851:
1849:
1846:
1844:
1843:
1839:
1837:
1834:
1832:
1829:
1827:
1824:
1822:
1821:RD-215 to 219
1819:
1817:
1814:
1812:
1809:
1807:
1804:
1802:
1799:
1797:
1796:RD-0233, 0234
1794:
1792:
1789:
1787:
1786:RD-0207, 0214
1784:
1782:
1779:
1777:
1774:
1773:
1771:
1766:
1765:Paektusan LRE
1763:
1762:
1760:
1756:
1753:
1752:
1750:
1746:
1743:
1741:
1738:
1737:
1735:
1731:
1728:
1726:
1723:
1721:
1718:
1716:
1713:
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165:Configuration
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159:Gas Generator
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967:solid motors
874:
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857:. Retrieved
846:
828:
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795:. Retrieved
791:the original
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770:. Retrieved
766:the original
756:
745:. Retrieved
721:the original
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668:the original
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613:
584:. Retrieved
580:the original
555:the original
442:
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345:
338:S.A. Kosberg
332:
302:
298:
294:
290:
288:
268:and on most
73:Manufacturer
55:First flight
2298:Engines in
1945:RD-109, 119
1883:RD-864, 869
1868:RD-854, 861
1831:RD-253, 275
1479:RD-170, 171
698:. July 2005
609:Yang, Vigor
218:326 seconds
178:Performance
108:Predecessor
91:Associated
86:Upper Stage
83:Application
2316:Categories
1685:YF-1, 2, 3
1633:Hypergolic
1605:Rutherford
1324:Prometheus
1286:Archimedes
859:2015-05-30
819:2015-05-30
797:2015-05-29
772:2015-05-30
747:2015-05-29
702:2015-05-29
642:2015-05-30
586:2015-05-29
535:References
431:Production
354:SS-8 Sasin
281:References
276:References
231:Dimensions
133:Propellant
58:1965-10-05
2226:Castor 30
2106:Zefiro 40
2101:Zefiro 23
2042:SpaB-140C
1439:NK-33, 44
1349:cryogenic
1195:Methalox
1014:Hydrolox
1006:Cryogenic
762:"RD-0106"
741:"RD-0110"
576:"RD-0107"
504:Molniya-M
465:RD-0110 (
454:RD-0108 (
447:RD-0107 (
388:Molniya-M
223:Burn time
98:Molniya-M
2241:Orbus-21
2096:Zefiro 9
1859:Ukraine
1637:Aerozine
1625:Storable
1517:Ukraine
1459:RD-0110R
1356:Kerolox
913:Archived
838:Archived
611:(eds.).
528:RD-0110R
498:See also
439:Versions
386:For the
363:Block-E
315:kerosene
309:burning
252:Dry mass
244:Diameter
215:, vacuum
203:pressure
201:Chamber
63:Designer
2300:italics
2261:Star 48
2256:Star 37
2236:Orbus-6
2157:Israel
2091:Waxwing
2047:Europe
2039:SpaB-65
1941:Russia
1806:RD-0237
1801:RD-0236
1772:Russia
1751:Israel
1711:Europe
1555:Kestrel
1501:S1.5400
1464:RD-0124
1430:Russia
1423:SCE-200
1319:Europe
1312:RD-0169
1307:Russia
1233:Longyun
1226:Lingyun
1144:RD-0146
1138:RD-0120
1129:Russia
1086:Vulcain
1072:Europe
995:Liquid
971:orbital
460:Voskhod
400:RD-0124
392:RD-0110
380:RD-0108
376:Voskhod
369:RD-0109
365:RD-0105
346:RD-0107
342:Molniya
334:OKB-154
329:History
305:) is a
299:RD-0108
291:RD-0110
260:Used in
170:Chamber
112:RD-0108
31:RD-0110
18:RD-0108
2216:AJ-60A
2181:KM-V2b
2172:Japan
2146:Salman
2112:India
2086:Topaze
2051:Mage 1
2016:China
2007:Solid
1914:TR-201
1878:RD-856
1873:RD-855
1863:RD-843
1853:S5.98M
1842:RD-270
1736:India
1730:Viking
1720:Astris
1715:Aestus
1705:YF-50D
1681:China
1590:RS-27A
1580:Merlin
1570:LR-105
1534:RD-810
1527:RD-801
1511:TEPREL
1507:Spain
1495:RD-193
1484:RD-180
1474:RD-120
1418:India
1411:Welkin
1404:YF-130
1398:YF-115
1393:YF-102
1388:YF-100
1372:China
1300:Aeon R
1293:Aeon 1
1280:Raptor
1264:YF-215
1257:YF-209
1250:TQ-15A
1214:China
1107:Japan
1096:CE-7.5
1092:India
1047:YF-75D
1033:China
885:
633:
410:Design
361:Vostok
303:RD-461
236:Length
118:Status
2281:X-254
2276:X-248
2266:UA120
2246:Orion
2221:Algol
2206:SRB-A
2201:M-34c
2176:KM-V1
2166:RSA-3
2142:Iran
2035:FG-47
2030:FG-46
2025:FG-36
2020:FG-02
1981:XLR81
1975:RS-88
1970:Curie
1960:Gamma
1935:Other
1919:XLR81
1908:RS-88
1903:LR-91
1898:LR-87
1848:S5.92
1776:17D61
1745:Vikas
1725:Vexin
1700:YF-40
1695:YF-23
1668:, or
1648:, or
1642:UH 25
1610:XLR50
1595:RS-56
1585:RS-27
1565:LR-89
1560:LR-79
1444:RD-58
1434:NK-15
1382:TH-12
1376:TH-11
1347:Semi-
1244:TQ-12
1239:TQ-11
1219:BF-20
1184:RS-68
1179:RS-25
1156:BE-3U
1101:CE-20
1081:Vinci
1065:YF-90
1058:YF-79
1052:YF-77
1042:YF-75
1037:YF-73
692:(PDF)
516:KBKhA
471:Soyuz
396:Soyuz
317:in a
226:250 s
196:74.36
155:Cycle
102:Soyuz
67:KBKhA
2271:SRMU
2196:M-34
2191:M-24
2186:M-14
2161:LK-1
2151:Rafe
2136:S200
2131:S139
2081:P230
2076:P120
2009:fuel
1893:AJ10
1755:LK-4
1650:UDMH
1600:S-3D
1521:RD-8
1360:RP-1
1331:M-10
1275:BE-4
1174:RL10
1163:BE-7
1122:LE-9
1116:LE-7
1111:LE-5
1076:HM7B
997:fuel
969:for
965:and
883:ISBN
879:AIAA
696:AIAA
631:ISBN
619:AIAA
491:2.1a
467:GRAU
456:GRAU
449:GRAU
404:2.1b
357:ICBM
350:GRAU
313:and
295:RO-8
293:(or
289:The
141:RG-1
100:and
49:USSR
2231:GEM
2126:S12
2071:P80
2066:PAP
2061:P-6
2056:P-4
1956:UK
1740:PS4
1670:HNO
1666:MON
1646:MMH
1550:H-1
1545:F-1
1364:LOX
1206:LOX
1169:J-2
1025:LOX
623:doi
336:of
150:2.2
137:LOX
2318::
2121:S9
2116:S7
1664:,
1653:/
1644:,
1639:,
1362:/
1204:/
1199:CH
1023:/
1018:LH
877:.
729:^
694:.
676:^
651:^
629:.
617:.
595:^
563:^
542:^
487:FG
483:U2
301:,
297:,
139:/
93:LV
1983:*
1977:*
1921:*
1910:*
1675:)
1672:3
1661:4
1659:O
1657:2
1655:N
1635:(
1366:)
1358:(
1208:)
1201:4
1197:(
1027:)
1020:2
1016:(
955:e
948:t
941:v
891:.
862:.
822:.
800:.
775:.
750:.
705:.
645:.
625::
589:.
489:/
485:/
481:/
479:U
477:/
475:L
473:/
367:/
173:4
20:)
Text is available under the Creative Commons Attribution-ShareAlike License. Additional terms may apply.
