Knowledge (XXG)

LE-9

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The LE-9 was operated successfully for the first time, on March 7, 2023. The second stage of that rocket, did not ignite and the mission was a failure. On February 17, 2024, the second launch of H3 was successful and LE-9 operations were successful for the second consecutive time.
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engine. However, it is physically difficult for an expander bleed cycle engine to generate large thrust, so the development of the LE-9 engine with a thrust of 1,471 kN (331,000 lb
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Kumada, Nobuhiko; Ogawara, Akira; Manako, Hiroyasu; Onga, Tadaoki; Sunakawa, Hideo; Kurosu, Akihide; Iizuka, Nobuyuki; Noda, Keiichiro; Okita, Koichi (2010-07-26).
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Watanabe, Daiki; Imai, Kazuhiro; Ogawara, Akira; Yamanishi, Nobuhiro; Neghishi, Hideyo; Kawatsu, Kaname; Kurosu, Akihide; Noda, Keiichiro (2011-07-31).
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The newly developed LE-9 engine is the most important factor in achieving cost reduction, improved safety and increased thrust. The
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Daiki, Watanabe; Manako, Hiroyasu; Onga, Tadaoki; Tamura, Takashi; Ikeda, Kazufumi; Isono, Mitsunori (December 2016).
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used in the LE-9 engine is a highly reliable combustion method that Japan has put into practical use for the
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Atsumi, Masahiro; Yoshikawa, Kimito; Ogawara, Akira; Onga, Tadaoki (December 2011).
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2022 or later, citing technical problems regarding the first stage LE-9 engine.
1478: 1939: 1934: 1854: 1839: 1824: 1528: 1232: 178: 2069:* Different versions of the engine use different propellant combinations 486: 420: 2034: 1859: 1834: 1829: 1589: 1584: 1579: 1574: 1569: 1564: 1559: 1554: 1498: 1274: 1237: 1227: 1222: 1196: 1085: 972: 917: 911: 1989: 1723: 1718: 1687: 1656: 1651: 1646: 1641: 1636: 1626: 1615: 1609: 1604: 1599: 1594: 1538: 1488: 1363: 1307: 1300: 1284: 1268: 1262: 1257: 1252: 1247: 1242: 1177: 1171: 1161: 1037: 1030: 869: 820: 468:"Application of High Fidelity Simulation to LE-X Engine Development" 2094: 2039: 1979: 1808: 1803: 1798: 1793: 1754: 1748: 1692: 1681: 1671: 1621: 1473: 1463: 1415: 1383: 1368: 1358: 1217: 1212: 1207: 1155: 1149: 1023: 1017: 1012: 992: 957: 952: 929: 906: 874: 838: 831: 825: 815: 810: 301:
On 21 January 2022, the launch of the first H3 was rescheduled to
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47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
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Firing tests of the LE-9 first-stage engine began in April 2017.
1676: 1666: 1458: 1294: 1133: 1048: 947: 936: 889: 884: 849: 572: 402:"Highly Reliable Design Approaches for Next Booster Engine LE-X" 328: 323: 288: 284: 38: 709: 1969: 1964: 1959: 1949: 678: 295:) is the most challenging and important development element. 272:. Two or three will be used to power the core stage of the 2106: 1779: 1708: 1405: 1398: 1129: 1120: 968: 787: 778: 767: 237: 232: 219: 211: 203: 198: 187: 176: 166: 158: 153: 145: 137: 132: 122: 114: 100: 93: 85: 75: 62: 54: 44: 34: 24: 694:Mitsubishi Heavy Industries Ltd. Rocket Engines 395: 393: 2126: 721: 352: 350: 8: 19: 341:Japanese Knowledge (XXG) LE-X (in Japanese) 2133: 2119: 1402: 1126: 784: 775: 728: 714: 706: 597:(in Japanese). Mynavi news. Archived from 2157:Rocket engines using hydrogen propellant 567:[2020: H3 projected debut date] 16:Japanese hydrolox expander rocket engine 2162:Rocket engines using the expander cycle 346: 593:Shinya Torishima (24 September 2020). 64: 18: 643:(in Japanese). JAXA. January 21, 2022 595:"H3ロケット開発を襲った"魔物"とは?、エンジンに見つかった技術的課題" 7: 2091: 2089: 759:Comparison of orbital rocket engines 617:(in Japanese). JAXA. Archived from 2105:. You can help Knowledge (XXG) by 14: 2093: 1770: 359:"Development of the LE-X Engine" 162:1,471 kN (331,000 lbf) 183:10.0 MPa (1,450 psi) 1: 1555:RD-0202 to 0206, 0208 to 0213 2101:This rocketry article is a 194:426 s (4.18 km/s) 49:Mitsubishi Heavy Industries 2183: 2088: 539:(4): 28–35. Archived from 372:(4): 36–43. Archived from 215:2.4 t (5,300 lb) 2065: 1768: 754: 224: 613: 2152:Rocket engines of Japan 1600:RD-250 to 252, 261, 262 641:"H3ロケットの試験機1号機の打上げについて" 168:Thrust-to-weight ratio 2076:are under development 1464:YF-20, 21, 22, 24, 25 1243:RD-107, 108, 117, 118 533:MHI Technical Review 366:MHI Technical Review 281:expander bleed cycle 270:expander bleed cycle 127:Expander Bleed cycle 1565:RD-0216, 0217, 0235 1228:RD-0107, 0108, 0110 565:"2020年:H3ロケットの目指す姿" 487:10.2514/6.2011-5930 421:10.2514/6.2010-6853 21: 699:2015-07-10 at the 681:. 17 February 2024 676:打ち上げ成功 前回の失敗乗り越える. 601:on 1 October 2020. 481:(AIAA 2011-5930). 415:(AIAA 2010-6853). 95:Liquid-fuel engine 2114: 2113: 2083: 2082: 2025:Space Shuttle SRB 1766: 1765: 1704: 1703: 1394: 1393: 1116: 1115: 496:978-1-60086-949-5 430:978-1-60086-958-7 319:H3 Launch Vehicle 244: 243: 226:H3 Launch Vehicle 70:H3 Launch Vehicle 25:Country of origin 2174: 2135: 2128: 2121: 2097: 2090: 1774: 1773: 1610:RD-263, 268, 273 1541:along other LREs 1403: 1263:RD-191, 151, 181 1127: 785: 776: 730: 723: 716: 707: 682: 673: 667: 666: 659: 653: 652: 650: 648: 637: 631: 630: 628: 626: 609: 603: 602: 590: 584: 583: 581: 580: 570: 561: 555: 554: 552: 551: 545: 530: 521: 515: 514: 512: 511: 505: 499:. Archived from 472: 463: 457: 456: 454: 453: 447: 441:. Archived from 406: 397: 388: 387: 385: 384: 378: 363: 354: 276:launch vehicle. 189:Specific impulse 66: 58:sustainer engine 22: 2182: 2181: 2177: 2176: 2175: 2173: 2172: 2171: 2142: 2141: 2140: 2139: 2086: 2084: 2079: 2061: 1782: 1775: 1771: 1762: 1700: 1590:RD-0255 to 0257 1585:RD-0243 to 0245 1447: 1436: 1432: 1426: 1414: 1390: 1131: 1122: 1112: 976: 970: 964: 795: 789: 770: 763: 750: 748:launch vehicles 734: 701:Wayback Machine 690: 685: 674: 670: 661: 660: 656: 646: 644: 639: 638: 634: 624: 622: 621:on 1 March 2020 615: 611: 610: 606: 592: 591: 587: 578: 576: 571:(in Japanese). 568: 563: 562: 558: 549: 547: 543: 528: 523: 522: 518: 509: 507: 503: 497: 470: 465: 464: 460: 451: 449: 445: 431: 404: 399: 398: 391: 382: 380: 376: 361: 356: 355: 348: 337: 315: 294: 262:liquid hydrogen 109:Liquid hydrogen 17: 12: 11: 5: 2180: 2178: 2170: 2169: 2167:Rocketry stubs 2164: 2159: 2154: 2144: 2143: 2138: 2137: 2130: 2123: 2115: 2112: 2111: 2098: 2081: 2080: 2078: 2077: 2070: 2066: 2063: 2062: 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Retrieved 374:the original 369: 365: 307: 300: 297: 278: 247: 245: 146:Nozzle ratio 45:Manufacturer 2072:Engines in 1719:RD-109, 119 1657:RD-864, 869 1642:RD-854, 861 1605:RD-253, 275 1253:RD-170, 171 647:January 21, 228:core stage. 154:Performance 76:Predecessor 63:Associated 55:Application 2146:Categories 1459:YF-1, 2, 3 1407:Hypergolic 1379:Rutherford 1098:Prometheus 1060:Archimedes 625:21 January 579:2015-07-08 550:2017-06-29 510:2015-07-08 452:2015-07-08 383:2015-07-08 335:References 238:References 233:References 199:Dimensions 101:Propellant 2000:Castor 30 1880:Zefiro 40 1875:Zefiro 23 1816:SpaB-140C 1213:NK-33, 44 1123:cryogenic 969:Methalox 788:Hydrolox 780:Cryogenic 614:LE-9 燃焼試験 439:110462567 255:cryogenic 2015:Orbus-21 1870:Zefiro 9 1633:Ukraine 1411:Aerozine 1399:Storable 1291:Ukraine 1233:RD-0110R 1130:Kerolox 697:Archived 313:See also 260:burning 212:Dry mass 191:, vacuum 179:pressure 177:Chamber 35:Designer 2074:italics 2035:Star 48 2030:Star 37 2010:Orbus-6 1931:Israel 1865:Waxwing 1821:Europe 1813:SpaB-65 1715:Russia 1580:RD-0237 1575:RD-0236 1546:Russia 1525:Israel 1485:Europe 1329:Kestrel 1275:S1.5400 1238:RD-0124 1204:Russia 1197:SCE-200 1093:Europe 1086:RD-0169 1081:Russia 1007:Longyun 1000:Lingyun 918:RD-0146 912:RD-0120 903:Russia 860:Vulcain 846:Europe 769:Liquid 745:orbital 220:Used in 138:Chamber 1990:AJ-60A 1955:KM-V2b 1946:Japan 1920:Salman 1886:India 1860:Topaze 1825:Mage 1 1790:China 1781:Solid 1688:TR-201 1652:RD-856 1647:RD-855 1637:RD-843 1627:S5.98M 1616:RD-270 1510:India 1504:Viking 1494:Astris 1489:Aestus 1479:YF-50D 1455:China 1364:RS-27A 1354:Merlin 1344:LR-105 1308:RD-810 1301:RD-801 1285:TEPREL 1281:Spain 1269:RD-193 1258:RD-180 1248:RD-120 1192:India 1185:Welkin 1178:YF-130 1172:YF-115 1167:YF-102 1162:YF-100 1146:China 1074:Aeon R 1067:Aeon 1 1054:Raptor 1038:YF-215 1031:YF-209 1024:TQ-15A 988:China 881:Japan 870:CE-7.5 866:India 821:YF-75D 807:China 493:  437:  427:  268:in an 252:liquid 204:Length 86:Status 2055:X-254 2050:X-248 2040:UA120 2020:Orion 1995:Algol 1980:SRB-A 1975:M-34c 1950:KM-V1 1940:RSA-3 1916:Iran 1809:FG-47 1804:FG-46 1799:FG-36 1794:FG-02 1755:XLR81 1749:RS-88 1744:Curie 1734:Gamma 1709:Other 1693:XLR81 1682:RS-88 1677:LR-91 1672:LR-87 1622:S5.92 1550:17D61 1519:Vikas 1499:Vexin 1474:YF-40 1469:YF-23 1442:, or 1422:, or 1416:UH 25 1384:XLR50 1369:RS-56 1359:RS-27 1339:LR-89 1334:LR-79 1218:RD-58 1208:NK-15 1156:TH-12 1150:TH-11 1121:Semi- 1018:TQ-12 1013:TQ-11 993:BF-20 958:RS-68 953:RS-25 930:BE-3U 875:CE-20 855:Vinci 839:YF-90 832:YF-79 826:YF-77 816:YF-75 811:YF-73 569:(PDF) 544:(PDF) 529:(PDF) 504:(PDF) 471:(PDF) 446:(PDF) 435:S2CID 405:(PDF) 377:(PDF) 362:(PDF) 285:LE-5A 250:is a 207:3.8 m 172:62.50 123:Cycle 80:LE-7A 29:Japan 2103:stub 2045:SRMU 1970:M-34 1965:M-24 1960:M-14 1935:LK-1 1925:Rafe 1910:S200 1905:S139 1855:P230 1850:P120 1783:fuel 1667:AJ10 1529:LK-4 1424:UDMH 1374:S-3D 1295:RD-8 1134:RP-1 1105:M-10 1049:BE-4 948:RL10 937:BE-7 896:LE-9 890:LE-7 885:LE-5 850:HM7B 771:fuel 743:for 739:and 649:2022 627:2020 573:JAXA 491:ISBN 425:ISBN 329:LE-5 324:LE-7 264:and 248:LE-9 246:The 149:37:1 39:JAXA 20:LE-9 2005:GEM 1900:S12 1845:P80 1840:PAP 1835:P-6 1830:P-4 1730:UK 1514:PS4 1444:HNO 1440:MON 1420:MMH 1324:H-1 1319:F-1 1138:LOX 980:LOX 943:J-2 799:LOX 679:NHK 483:doi 417:doi 118:5.9 2148:: 1895:S9 1890:S7 1438:, 1427:/ 1418:, 1413:, 1136:/ 978:/ 973:CH 797:/ 792:LH 537:53 535:. 531:. 489:. 479:47 477:. 473:. 433:. 423:. 413:46 411:. 407:. 392:^ 370:48 368:. 364:. 349:^ 303:FY 274:H3 107:/ 65:LV 2134:e 2127:t 2120:v 2109:. 1757:* 1751:* 1695:* 1684:* 1449:) 1446:3 1435:4 1433:O 1431:2 1429:N 1409:( 1140:) 1132:( 982:) 975:4 971:( 801:) 794:2 790:( 729:e 722:t 715:v 665:. 651:. 629:. 582:. 553:. 513:. 485:: 455:. 419:: 386:. 293:f 289:B 287:/ 141:1

Index

Japan
JAXA
Mitsubishi Heavy Industries
H3 Launch Vehicle
LE-7A
Liquid-fuel engine
Liquid oxygen
Liquid hydrogen
Expander Bleed cycle
Thrust-to-weight ratio
pressure
Specific impulse
H3 Launch Vehicle
liquid
cryogenic
rocket engine
liquid hydrogen
liquid oxygen
expander bleed cycle
H3
expander bleed cycle
LE-5A
B
FY
H3 Launch Vehicle
LE-7
LE-5
Japanese Knowledge (XXG) LE-X (in Japanese)

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