Knowledge (XXG)

YF-90

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cycle. It is China's first hydrogen-oxygen engine to use the staged combustion cycle and is expected to be used for the second stage of the Long March 9, which is a three-stage rocket with boosters. The engine has advanced features such as variable thrust, multiple ignitions, and automatic fault
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On September 23, 2021, the engine successfully underwent its first semi-system test. The YF -90 engine is one of the key technologies for China's deep space exploration ambitions.
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On July 28, 2021, the engine's manufacturer, China Aerospace Science and Technology Corporation (CASC) completed the first YF-90 engineering prototype.
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engine. The YF-130 is a liquid kerosene-oxygen rocket engine with a thrust of 500 tonnes. Both engines are expected to be ready for flight by 2025.
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In 2023, CASC plans to conduct more tests on the YF-90 engine, as well as on its first-stage counterpart, the
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Tech" 1863: 1803: 1632: 1627: 1622: 1617: 1578: 1572: 1516: 1505: 1495: 1445: 1297: 1287: 1239: 1207: 1192: 1182: 1041: 1036: 1031: 979: 973: 847: 841: 836: 816: 781: 776: 753: 730: 698: 655: 649: 639: 634: 51: 28: 1500: 1490: 1282: 1118: 957: 872: 771: 760: 719: 713: 708: 673: 533: 1793: 1788: 1783: 1773: 463:"China moves to next stage of super heavy rocket development" 376:"China successfully tests new engine for Long March 9 rocket" 1603: 1532: 1229: 1222: 953: 944: 792: 611: 602: 591: 199: 194: 186: 178: 168: 163: 152: 142: 130: 125: 117: 112: 104: 94: 86: 72: 65: 57: 47: 34: 24: 1930:Rocket engines using the staged combustion cycle 545: 8: 401:Journal of Mechanical Science and Technology 360:: CS1 maint: multiple names: authors list ( 320:: CS1 maint: multiple names: authors list ( 303:(in Simplified Chinese). 北京航天动力研究所,北京 100076 19: 1226: 950: 608: 599: 552: 538: 530: 412: 339:(in Simplified Chinese). 《火箭推进》2022年02期. 1920:Rocket engines using hydrogen propellant 294: 292: 262: 353: 313: 299:丁兆波,刘 倩,王天泰,杨继东,孙纪国,龚杰峰 (2020-11-17). 36: 18: 507: 505: 7: 583:Comparison of orbital rocket engines 487:(in Simplified Chinese). 北京航天动力研究所. 134:2,200 kilonewtons (490,000 lb 14: 485:"重型运载火箭220吨级补燃循环氢氧发动机首次半系统试验圆满成功" 182:2.87 metres (9 ft 5 in) 16:Chinese liquid-fuel rocket engine 1594: 440:(in Traditional Chinese). 香港01. 190:4,800 kilograms (10,600 lb) 491:from the original on 2021-09-27 444:from the original on 2021-08-06 438:"中國製造|重型火箭220噸級引擎現身 首台工程樣機完成生產" 343:from the original on 2022-06-05 335:孙纪国,郑孟伟,龚杰峰,陶瑞峰 (2022-01-15). 1: 1379:RD-0202 to 0206, 0208 to 0213 272:"China's new rocket engines" 159:453 seconds (4.44 km/s) 1946: 414:10.1007/s42405-022-00519-7 1889: 1592: 578: 1925:Rocket engines of China 1424:RD-250 to 252, 261, 262 172:6.1 metres (20 ft) 99:Staged combustion cycle 144:Thrust-to-weight ratio 1900:are under development 1288:YF-20, 21, 22, 24, 25 1067:RD-107, 108, 117, 118 301:"220t级补燃循环氢氧发动机推力室研制" 337:"220tf补燃循环氢氧发动机研制进展" 1389:RD-0216, 0217, 0235 1052:RD-0107, 0108, 0110 174:(With Engine Mount) 21: 483:郑孟伟 (2021-09-27). 436:蘇子牧 (2021-07-29). 90:6.0 (±5%) Variable 67:Liquid-fuel engine 1907: 1906: 1849:Space Shuttle SRB 1590: 1589: 1528: 1527: 1218: 1217: 940: 939: 270:Brügge, Norbert. 232:staged combustion 206: 205: 25:Country of origin 1937: 1598: 1597: 1434:RD-263, 268, 273 1365:along other LREs 1227: 1087:RD-191, 151, 181 951: 609: 600: 554: 547: 540: 531: 524: 523: 521: 520: 509: 500: 499: 497: 496: 480: 474: 473: 471: 470: 459: 453: 452: 450: 449: 433: 427: 426: 416: 407:(2): 1015–1026. 393: 387: 386: 384: 383: 372: 366: 365: 359: 351: 349: 348: 332: 326: 325: 319: 311: 309: 308: 296: 287: 286: 284: 282: 267: 154:Specific impulse 38: 22: 1945: 1944: 1940: 1939: 1938: 1936: 1935: 1934: 1910: 1909: 1908: 1903: 1885: 1606: 1599: 1595: 1586: 1524: 1414:RD-0255 to 0257 1409:RD-0243 to 0245 1271: 1260: 1256: 1250: 1238: 1214: 955: 946: 936: 800: 794: 788: 619: 613: 594: 587: 574: 572:launch vehicles 558: 528: 527: 518: 516: 511: 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1363:Paektusan LRE 1361: 1360: 1358: 1354: 1351: 1350: 1348: 1344: 1341: 1339: 1336: 1335: 1333: 1329: 1326: 1324: 1321: 1319: 1316: 1314: 1311: 1310: 1308: 1304: 1301: 1299: 1296: 1294: 1291: 1289: 1286: 1284: 1281: 1280: 1278: 1277: 1275: 1272: 1265: 1261: 1249: 1245: 1241: 1236: 1232: 1228: 1225: 1221: 1209: 1206: 1204: 1201: 1199: 1196: 1194: 1191: 1189: 1186: 1184: 1181: 1179: 1176: 1174: 1171: 1169: 1166: 1164: 1161: 1159: 1156: 1154: 1151: 1149: 1146: 1144: 1141: 1140: 1138: 1134: 1133: 1129: 1127: 1126: 1122: 1120: 1117: 1116: 1114: 1110: 1107: 1106: 1104: 1100: 1097: 1095: 1094: 1090: 1088: 1085: 1083: 1080: 1078: 1075: 1073: 1070: 1068: 1065: 1063: 1060: 1058: 1055: 1053: 1050: 1048: 1047:RD-0105, 0109 1045: 1043: 1040: 1038: 1035: 1033: 1030: 1029: 1027: 1023: 1022: 1018: 1017: 1015: 1011: 1010: 1006: 1004: 1003: 999: 997: 994: 992: 989: 987: 984: 982: 981: 977: 975: 972: 971: 969: 968: 966: 963: 959: 952: 949: 943: 931: 930: 926: 924: 923: 919: 918: 916: 912: 911: 907: 906: 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221: 220:rocket engine 218: 215: 211: 202: 198: 193: 189: 185: 181: 177: 171: 167: 162: 158: 155: 151: 147: 145: 141: 133: 129: 124: 120: 116: 113:Configuration 111: 107: 103: 100: 97: 93: 89: 87:Mixture ratio 85: 82: 78: 77:Liquid oxygen 75: 71: 68: 64: 60: 56: 53: 50: 46: 43: 40: 33: 30: 27: 23: 1897: 1438: 1359:North Korea 1130: 1123: 1091: 1019: 1007: 1000: 978: 927: 920: 908: 896: 889: 882: 860: 853: 846: 829: 822: 815: 759: 752: 740: 718: 662: 661: 654: 565:solid motors 517:. 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Retrieved 275: 265: 248: 245: 242: 209: 207: 118:Nozzle ratio 42:Long March 9 1896:Engines in 1543:RD-109, 119 1481:RD-864, 869 1466:RD-854, 861 1429:RD-253, 275 1077:RD-170, 171 235:diagnosis. 126:Performance 48:Predecessor 35:Associated 1914:Categories 1283:YF-1, 2, 3 1231:Hypergolic 1203:Rutherford 922:Prometheus 884:Archimedes 519:2023-03-08 495:2021-09-27 469:2023-03-08 448:2021-08-07 382:2023-03-08 347:2022-06-05 307:2022-04-01 257:References 200:References 195:References 164:Dimensions 73:Propellant 1824:Castor 30 1704:Zefiro 40 1699:Zefiro 23 1640:SpaB-140C 1037:NK-33, 44 947:cryogenic 793:Methalox 612:Hydrolox 604:Cryogenic 423:251938449 217:cryogenic 1839:Orbus-21 1694:Zefiro 9 1457:Ukraine 1235:Aerozine 1223:Storable 1115:Ukraine 1057:RD-0110R 954:Kerolox 489:Archived 442:Archived 356:cite web 341:Archived 316:cite web 222:burning 187:Dry mass 179:Diameter 156:, vacuum 1898:italics 1859:Star 48 1854:Star 37 1834:Orbus-6 1755:Israel 1689:Waxwing 1645:Europe 1637:SpaB-65 1539:Russia 1404:RD-0237 1399:RD-0236 1370:Russia 1349:Israel 1309:Europe 1153:Kestrel 1099:S1.5400 1062:RD-0124 1028:Russia 1021:SCE-200 917:Europe 910:RD-0169 905:Russia 831:Longyun 824:Lingyun 742:RD-0146 736:RD-0120 727:Russia 684:Vulcain 670:Europe 593:Liquid 569:orbital 281:8 March 239:History 1814:AJ-60A 1779:KM-V2b 1770:Japan 1744:Salman 1710:India 1684:Topaze 1649:Mage 1 1614:China 1605:Solid 1512:TR-201 1476:RD-856 1471:RD-855 1461:RD-843 1451:S5.98M 1440:RD-270 1334:India 1328:Viking 1318:Astris 1313:Aestus 1303:YF-50D 1279:China 1188:RS-27A 1178:Merlin 1168:LR-105 1132:RD-810 1125:RD-801 1109:TEPREL 1105:Spain 1093:RD-193 1082:RD-180 1072:RD-120 1016:India 1009:Welkin 1002:YF-130 996:YF-115 991:YF-102 986:YF-100 970:China 898:Aeon R 891:Aeon 1 878:Raptor 862:YF-215 855:YF-209 848:TQ-15A 812:China 705:Japan 694:CE-7.5 690:India 645:YF-75D 631:China 421:  251:YF-130 214:liquid 169:Length 58:Status 1879:X-254 1874:X-248 1864:UA120 1844:Orion 1819:Algol 1804:SRB-A 1799:M-34c 1774:KM-V1 1764:RSA-3 1740:Iran 1633:FG-47 1628:FG-46 1623:FG-36 1618:FG-02 1579:XLR81 1573:RS-88 1568:Curie 1558:Gamma 1533:Other 1517:XLR81 1506:RS-88 1501:LR-91 1496:LR-87 1446:S5.92 1374:17D61 1343:Vikas 1323:Vexin 1298:YF-40 1293:YF-23 1266:, or 1246:, or 1240:UH 25 1208:XLR50 1193:RS-56 1183:RS-27 1163:LR-89 1158:LR-79 1042:RD-58 1032:NK-15 980:TH-12 974:TH-11 945:Semi- 842:TQ-12 837:TQ-11 817:BF-20 782:RS-68 777:RS-25 754:BE-3U 699:CE-20 679:Vinci 663:YF-90 656:YF-79 650:YF-77 640:YF-75 635:YF-73 419:S2CID 230:in a 212:is a 210:YF-90 105:Pumps 95:Cycle 52:YF-77 29:China 20:YF-90 1869:SRMU 1794:M-34 1789:M-24 1784:M-14 1759:LK-1 1749:Rafe 1734:S200 1729:S139 1679:P230 1674:P120 1607:fuel 1491:AJ10 1353:LK-4 1248:UDMH 1198:S-3D 1119:RD-8 958:RP-1 929:M-10 873:BE-4 772:RL10 761:BE-7 720:LE-9 714:LE-7 709:LE-5 674:HM7B 595:fuel 567:for 563:and 362:link 322:link 283:2023 226:and 208:The 148:46.7 1829:GEM 1724:S12 1669:P80 1664:PAP 1659:P-6 1654:P-4 1554:UK 1338:PS4 1268:HNO 1264:MON 1244:MMH 1148:H-1 1143:F-1 962:LOX 804:LOX 767:J-2 623:LOX 409:doi 121:100 1916:: 1719:S9 1714:S7 1262:, 1251:/ 1242:, 1237:, 960:/ 802:/ 797:CH 621:/ 616:LH 504:^ 417:. 405:36 403:. 399:. 358:}} 354:{{ 318:}} 314:{{ 291:^ 274:. 79:/ 37:LV 1581:* 1575:* 1519:* 1508:* 1273:) 1270:3 1259:4 1257:O 1255:2 1253:N 1233:( 964:) 956:( 806:) 799:4 795:( 625:) 618:2 614:( 553:e 546:t 539:v 522:. 498:. 472:. 451:. 425:. 411:: 385:. 364:) 350:. 324:) 310:. 285:. 138:) 136:f 108:2

Index

China
Long March 9
YF-77
Liquid-fuel engine
Liquid oxygen
Liquid hydrogen
Staged combustion cycle
Thrust-to-weight ratio
Specific impulse
liquid
cryogenic
rocket engine
liquid hydrogen
liquid oxygen
staged combustion
YF-130
"China's new rocket engines"


"220t级补燃循环氢氧发动机推力室研制"
cite web
link
"220tf补燃循环氢氧发动机研制进展"
Archived
cite web
link
"China successfully tests new engine for Long March 9 rocket"
"Development Trend of Liquid Hydrogen-Fueled Rocket Engines (Part 1): Current Status and Future Prospects in Korea and China"
doi
10.1007/s42405-022-00519-7

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