Knowledge (XXG)

RD-0109

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It used a corrugated metal construction for the cooling jackets, with the lower section of the nozzle lacking an external liner, to save weight. This led to a 9.3% weight reduction even with the increased thrust. This new version was christened as the RD-0109 and entered service on the December 22, 1960, launch of a (
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Between 1959 and 1960 the engine was modified to improve reliability for crewed flight. Thrust was also increased 2%, thanks to improved injection elements. It also introduced an innovation attributed to S.A. Kosbergs in its construction, that has been a staple of Soviet (and later Russian) engines.
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probe, but ended 92 seconds after launch when the rocket broke up from longitudinal vibration, causing the strap-ons to separate from the vehicle, which then crashed downrange. Neither was successful the second flight of a Luna 8K72 (October 11, 1958), which was to launch the
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Since the February 20, 1958 order of development, it took nine months to develop the engine. It was done by using RD-0102 assemblies and combustion chamber. Fifty eight static tests were conducted with 27 engines.
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probe and ended 104 seconds after launch when the rocket again disintegrated from vibration. The third flight of a Luna 8K72 (December 4, 1958), which was to launch the
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Block-E. Regrettably, the gas generator of the rocket third stage suffered a failure and the RD-0109 could not prove itself in flight. That chance came with the second
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rocket and enable it to send useful payloads to those high energy destinations. This fourth stage was called Block-E, and its development started during 1958.
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On January 2, 1959, as part of the Luna 8K72's Block-E stage, the engine RD-0105 finally performed its first successful mission, the launch of
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and, while the spacecraft missed the Moon with which it was supposed to crash, it became the first human made object to enter a
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Index: 8D714), also known as RD-448 or RO-05. Was the first version but had some reliability issues. Used on the
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Improvement and modifications required to comply with the man rating of the RD-0105 led it to have two versions:
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probe, also ended 245 seconds after launch when the Block-I core stage shut down from loss of engine lubricant.
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Sutton, George Paul (November 2005). "8.5 KB Khimautomatiki or Chemical Automatics Design Bureau".
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Lardier, Christian; Barensky, Stefan (2013-03-12). "Chapter 3 - The Council of Chief Designers".
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RD-109 engine. Due to the complication of developing that latter, Kosberg got the contract.
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and the first spaceflight to send animals into orbit and return them safely back to Earth.
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design bureau initially competed two projects for the Block-E propulsion: 8K72, using the
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Lardier, Christian; Barensky, Stefan (2013-03-12). "Chapter 5 - The Various Versions".
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Index: 8D719). Improved and more reliable version which was used on the rest of the
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Russian Planetary Exploration: History, Development, Legacy and Prospects
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On April 12, 1961, the RD-0109, as part of the Block-E stage of the
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The Soyuz Launch Vehicle: The Two Lives of an Engineering Triumph
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The Soyuz Launch Vehicle: The Two Lives of an Engineering Triumph
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On December 22, 1960, the RD-0109 had its first flight on a
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Central Committee of the Communist Party of the Soviet Union
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launch, where the RD-0109 successfully launched the
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satellites could be done with the two stage booster
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proposing a bold plan to send robotic spacecraft to
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It was the first spacecraft 1147: 657:On September 14, 1959, the RD-0105 propelled 615:, to achieve escape velocity required by the 8: 2537:Rocket engines using the gas-generator cycle 959: 957: 955: 721:On June 16, 1963, the RD-0109 propelled the 263: 19: 1026:Magno Gomes de Paula, Victor (2009-08-30). 999:History of Liquid Propellant Rocket Engines 1828: 1552: 1210: 1201: 1154: 1140: 1132: 676:On August 19, 1960, the RD-0105 propelled 25: 2532:Rocket engines using kerosene propellant 808: 328: 262: 93: 18: 787:to be the first human to orbit Earth. 706:8K72K rocket, propelled the historic 7: 1185:Comparison of orbital rocket engines 793:- The RD-0105/RD-0109 design bureau. 905:. Springer-Praxis. pp. 24–25. 2527:Rocket engines of the Soviet Union 783:- The launch vehicle that enabled 718:and the first to orbit the Earth. 408:49.4 kilonewtons (11,100 lbf) 185:54.5 kilonewtons (12,300 lbf) 14: 592:The RD-0109 is the basis for the 2196: 729:the first woman to orbit Earth. 663:to reach the surface of the Moon 510:. It was the engine used on the 228:1,555 millimetres (61.2 in) 534:sent series of letters to the 504:gas generator combustion cycle 459:733 millimetres (28.9 in) 451:494 millimetres (19.4 in) 419:4.5 megapascals (650 psi) 236:733 millimetres (28.9 in) 1: 1981:RD-0202 to 0206, 0208 to 0213 607:While the first launches for 565:RD-0105, and the 8K73, using 972:. Springer-Praxis. pp.  934:. Springer-Praxis. pp.  196:5 megapascals (730 psi) 1048:Falcão, Duda (2010-02-26). 467:130 kilograms (290 lb) 244:121 kilograms (267 lb) 2558: 1119:Voronezh Mechanical Plant 680:mission. It was the third 2491: 2194: 1180: 1073:. NASA NSSDC. 2005-01-06. 797:Voronezh Mechanical Plant 714:the first human to go to 476: 313:Voronezh Mechanical Plant 253: 78:Voronezh Mechanical Plant 24: 2522:Rocket engines of Russia 2026:RD-250 to 252, 261, 262 1096:. KBKhA. Archived from 862:. KBKhA. Archived from 727:Valentina V. Tereshkova 1127:RSC Progress Home Page 901:Harvey, Brian (2007). 622:The first flight of a 594:Brazilian Space Agency 585:) spacecraft aboard a 514:Block-E that launched 2502:are under development 1890:YF-20, 21, 22, 24, 25 1669:RD-107, 108, 117, 118 526:After the success of 2542:KBKhA rocket engines 1991:RD-0216, 0217, 0235 1654:RD-0107, 0108, 0110 883:. Gunter Space Page 265: 21: 699:mission to orbit. 357:Liquid-fuel engine 134:Liquid-fuel engine 2509: 2508: 2451:Space Shuttle SRB 2192: 2191: 2130: 2129: 1820: 1819: 1542: 1541: 1100:on 24 March 2016. 1052:. Brazilian Space 1030:. Brazilian Space 912:978-0-387-46343-8 866:on 26 March 2016. 682:Vostok spacecraft 484: 483: 269:Country of origin 261: 260: 34:Country of origin 2549: 2200: 2199: 2036:RD-263, 268, 273 1967:along other LREs 1829: 1689:RD-191, 151, 181 1553: 1211: 1202: 1156: 1149: 1142: 1133: 1102: 1101: 1090: 1075: 1074: 1067: 1061: 1060: 1058: 1057: 1045: 1039: 1038: 1036: 1035: 1023: 1017: 1016: 994: 988: 987: 971: 961: 950: 949: 933: 923: 917: 916: 898: 892: 891: 889: 888: 877: 868: 867: 856: 710:to orbit making 697:Korabl-Sputnik 4 678:Korabl-Sputnik 2 599:engine project. 425:Specific impulse 330: 266: 202:Specific impulse 95: 29: 22: 2557: 2556: 2552: 2551: 2550: 2548: 2547: 2546: 2512: 2511: 2510: 2505: 2487: 2208: 2201: 2197: 2188: 2126: 2016:RD-0255 to 0257 2011:RD-0243 to 0245 1873: 1862: 1858: 1852: 1840: 1816: 1557: 1548: 1538: 1402: 1396: 1390: 1221: 1215: 1196: 1189: 1176: 1174:launch vehicles 1160: 1114:KbKhA Home Page 1110: 1105: 1092: 1091: 1078: 1069: 1068: 1064: 1055: 1053: 1047: 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195: 193: 188: 184: 180: 175: 171: 167: 164:Configuration 162: 159: 158:Gas Generator 156: 152: 149: 145: 142: 138: 135: 131: 127: 123: 120: 117: 113: 110: 107: 103: 100: 97: 90: 86: 82: 79: 76: 72: 69: 65: 62: 58: 54: 50: 46: 42: 39: 36: 32: 28: 23: 16:Rocket engine 2499: 2040: 1961:North Korea 1732: 1725: 1693: 1648: 1621: 1609: 1602: 1580: 1529: 1522: 1510: 1498: 1491: 1484: 1462: 1455: 1448: 1431: 1424: 1417: 1361: 1354: 1342: 1320: 1263: 1256: 1167:solid motors 1120: 1098:the original 1065: 1054:. Retrieved 1043: 1032:. Retrieved 1021: 998: 992: 967: 929: 921: 902: 896: 885:. Retrieved 864:the original 785:Yuri Gagarin 736: 720: 712:Yuri Gagarin 701: 686: 675: 667:State Emblem 656: 652:heliocentric 641: 621: 606: 591: 579: 575: 559:S.A. Kosberg 552: 525: 516:Yuri Gagarin 487: 485: 309:Manufacturer 303:S.A. Kosberg 279:First flight 74:Manufacturer 68:S.A. Kosberg 44:First flight 2498:Engines in 2145:RD-109, 119 2083:RD-864, 869 2068:RD-854, 861 2031:RD-253, 275 1679:RD-170, 171 716:outer space 522:Development 430:316 seconds 400:Performance 334:Vostok 8K72 327:Associated 322:Upper Stage 319:Application 287:Last flight 177:Performance 105:Predecessor 92:Associated 87:Upper Stage 84:Application 52:Last flight 2516:Categories 1885:YF-1, 2, 3 1833:Hypergolic 1805:Rutherford 1524:Prometheus 1486:Archimedes 1121:(Archived) 1056:2015-06-01 1034:2015-06-01 887:2015-06-01 804:References 553:Korolev's 518:to orbit. 443:Dimensions 363:Propellant 290:1960-12-01 282:1959-01-02 220:Dimensions 140:Propellant 55:1991-08-29 47:1960-12-22 2426:Castor 30 2306:Zefiro 40 2301:Zefiro 23 2242:SpaB-140C 1639:NK-33, 44 1549:cryogenic 1395:Methalox 1214:Hydrolox 1206:Cryogenic 756:RD-0109 ( 741:RD-0105 ( 624:Luna 8K72 609:Sputnik 1 528:Sputnik 1 435:Burn time 340:Successor 212:Burn time 115:Successor 2441:Orbus-21 2296:Zefiro 9 2059:Ukraine 1837:Aerozine 1825:Storable 1717:Ukraine 1659:RD-0110R 1556:Kerolox 881:"Vostok" 769:See also 751:Vostok-L 733:Versions 725:making 723:Vostok 6 708:Vostok 1 704:Vostok-K 693:Vostok-K 689:Vostok-K 587:Vostok-K 500:kerosene 494:burning 464:Dry mass 456:Diameter 427:, vacuum 415:pressure 413:Chamber 295:Designer 241:Dry mass 233:Diameter 204:, vacuum 192:pressure 190:Chamber 60:Designer 2500:italics 2461:Star 48 2456:Star 37 2436:Orbus-6 2357:Israel 2291:Waxwing 2247:Europe 2239:SpaB-65 2141:Russia 2006:RD-0237 2001:RD-0236 1972:Russia 1951:Israel 1911:Europe 1755:Kestrel 1701:S1.5400 1664:RD-0124 1630:Russia 1623:SCE-200 1519:Europe 1512:RD-0169 1507:Russia 1433:Longyun 1426:Lingyun 1344:RD-0146 1338:RD-0120 1329:Russia 1286:Vulcain 1272:Europe 1195:Liquid 1171:orbital 764:family. 669:of the 654:orbit. 613:Sputnik 603:History 589:8K72K. 571:OKB-456 567:Glushko 563:OKB-154 532:Korolev 508:RD-0105 488:RD-0109 480:Block-E 472:Used in 392:Chamber 351:Retired 343:RD-0109 299:OKB-154 264:RD-0105 257:Block-E 249:Used in 169:Chamber 128:Retired 119:RD-0108 109:RD-0105 64:OKB-154 20:RD-0109 2416:AJ-60A 2381:KM-V2b 2372:Japan 2346:Salman 2312:India 2286:Topaze 2251:Mage 1 2216:China 2207:Solid 2114:TR-201 2078:RD-856 2073:RD-855 2063:RD-843 2053:S5.98M 2042:RD-270 1936:India 1930:Viking 1920:Astris 1915:Aestus 1905:YF-50D 1881:China 1790:RS-27A 1780:Merlin 1770:LR-105 1734:RD-810 1727:RD-801 1711:TEPREL 1707:Spain 1695:RD-193 1684:RD-180 1674:RD-120 1618:India 1611:Welkin 1604:YF-130 1598:YF-115 1593:YF-102 1588:YF-100 1572:China 1500:Aeon R 1493:Aeon 1 1480:Raptor 1464:YF-215 1457:YF-209 1450:TQ-15A 1414:China 1307:Japan 1296:CE-7.5 1292:India 1247:YF-75D 1233:China 1009:  980:  942:  938:–145. 909:  781:Vostok 762:Vostok 659:Luna 2 644:Luna 1 583:Vostok 512:Vostok 478:Vostok 448:Length 348:Status 255:Vostok 225:Length 125:Status 99:Vostok 2481:X-254 2476:X-248 2466:UA120 2446:Orion 2421:Algol 2406:SRB-A 2401:M-34c 2376:KM-V1 2366:RSA-3 2342:Iran 2235:FG-47 2230:FG-46 2225:FG-36 2220:FG-02 2181:XLR81 2175:RS-88 2170:Curie 2160:Gamma 2135:Other 2119:XLR81 2108:RS-88 2103:LR-91 2098:LR-87 2048:S5.92 1976:17D61 1945:Vikas 1925:Vexin 1900:YF-40 1895:YF-23 1868:, or 1848:, or 1842:UH 25 1810:XLR50 1795:RS-56 1785:RS-27 1765:LR-89 1760:LR-79 1644:RD-58 1634:NK-15 1582:TH-12 1576:TH-11 1547:Semi- 1444:TQ-12 1439:TQ-11 1419:BF-20 1384:RS-68 1379:RS-25 1356:BE-3U 1301:CE-20 1281:Vinci 1265:YF-90 1258:YF-79 1252:YF-77 1242:YF-75 1237:YF-73 976:–88. 791:KBKhA 555:OKB-1 544:Venus 502:in a 490:is a 377:Cycle 154:Cycle 2471:SRMU 2396:M-34 2391:M-24 2386:M-14 2361:LK-1 2351:Rafe 2336:S200 2331:S139 2281:P230 2276:P120 2209:fuel 2093:AJ10 1955:LK-4 1850:UDMH 1800:S-3D 1721:RD-8 1560:RP-1 1531:M-10 1475:BE-4 1374:RL10 1363:BE-7 1322:LE-9 1316:LE-7 1311:LE-5 1276:HM7B 1197:fuel 1169:for 1165:and 1007:ISBN 1003:AIAA 978:ISBN 940:ISBN 907:ISBN 775:Luna 758:GRAU 749:and 747:Luna 743:GRAU 671:USSR 542:and 540:Mars 498:and 486:The 438:454s 371:RG-1 273:USSR 215:430s 148:RG-1 38:USSR 2431:GEM 2326:S12 2271:P80 2266:PAP 2261:P-6 2256:P-4 2156:UK 1940:PS4 1870:HNO 1866:MON 1846:MMH 1750:H-1 1745:F-1 1564:LOX 1406:LOX 1369:J-2 1225:LOX 936:140 597:L75 569:'s 561:'s 548:R-7 367:LOX 144:LOX 2518:: 2321:S9 2316:S7 1864:, 1853:/ 1844:, 1839:, 1562:/ 1404:/ 1399:CH 1223:/ 1218:LH 1079:^ 1001:. 974:87 954:^ 872:^ 811:^ 673:. 530:, 369:/ 329:LV 301:, 146:/ 94:LV 66:, 2183:* 2177:* 2121:* 2110:* 1875:) 1872:3 1861:4 1859:O 1857:2 1855:N 1835:( 1566:) 1558:( 1408:) 1401:4 1397:( 1227:) 1220:2 1216:( 1155:e 1148:t 1141:v 1059:. 1037:. 1015:. 986:. 948:. 915:. 890:. 395:1 172:1

Index


USSR
OKB-154
S.A. Kosberg
Voronezh Mechanical Plant
Vostok
RD-0105
RD-0108
Liquid-fuel engine
LOX
RG-1
Gas Generator
pressure
Specific impulse
Vostok
USSR
OKB-154
S.A. Kosberg
Voronezh Mechanical Plant
Vostok 8K72
Liquid-fuel engine
LOX
RG-1
Gas Generator
pressure
Specific impulse
Vostok
rocket engine
liquid oxygen
kerosene

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