Knowledge (XXG)

Rocketdyne LR-101

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Due to several modifications the LR-101 underwent over the years, there are many different variants of this engine. One of the first changes was the downrating of the engine to a lower thrust level, both because the engine provided far more thrust than required to steer the rocket and to save fuel
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in the vicinity of their primary engines to provide large arcs for the vernier thrusters. While the pair of LR-101s on the Atlas was mounted radially above the booster engines of the vehicle, on the Thor they were placed at the base of the vehicle.
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of the sustainer engine until it was shut off. After sustainer burnout, this pair of thrusters would switch to feed off the remaining propellant, effectively becoming a
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missile had planned on propelling his 'X-3 Volksrocket' with four Rocketdyne LR-101 engines, but despite many test firings the rocket never left the ground.
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utilized in American rocketry and has become a sought-after object for item collectors and
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for the main engines. Another major change was the replacement of the original
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Each of these rockets used two LR-101 secondary engines to provide
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LR-101 Thrust chamber on a gimbal mount designed by
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The pair of LR-101 444:"An Amateur Workhorse: The LR-101 Rocket Engine" 163:(Pressure-fed) 1,060 pounds-force (4,700 N) 199:(Pressure-fed) 209.8 seconds (2.057 km/s) 150:(Pressure-fed) 830 pounds-force (3,700 N) 1887: 485: 277:of the rocket before separating the payload. 261:would receive their propellant flow from the 8: 160:(Tank-fed) 1,017 pounds-force (4,520 N) 19: 1928:Rocket engines using the pressure-fed cycle 235:in the mid-to-late fifties and used in the 227:The LR-101 is a fixed thrust, single start 181:(Pressure-fed) 2.45 MPa (355 psi) 1894: 1880: 1166: 890: 548: 539: 492: 478: 470: 419:"Heroicrelics - Small engines for big job" 196:(Tank-fed) 198.7 seconds (1.949 km/s) 25: 334:On the 'Galactic Aztec', the engine used 1913:Rocket engines using kerosene propellant 16:Vernier thruster developed by Rocketdyne 385: 394:"Heroicrelics - LR-101 Vernier Engine" 178:(Tank-fed) 2.1 MPa (300 psi) 18: 315:The LR-101 is one of the most common 7: 1852: 1850: 523:Comparison of orbital rocket engines 369:- The first rocket to use the LR-101 1933:Rocket engines of the United States 375:- The designer bureau of the LR-101 1866:. You can help Knowledge (XXG) by 14: 194: 176: 158: 1854: 1534: 353:as well as the later commercial 1: 1319:RD-0202 to 0206, 0208 to 0213 311:Role in experimental rocketry 288:pyrotechnical ignition system 342:, which was utilized in the 1943:Spacecraft attitude control 1862:This rocketry article is a 338:as a propellant instead of 321:builders of amateur rockets 255:yaw, pitch and roll control 1964: 1849: 1829: 1532: 518: 218: 24: 290:with an igniter using a 1923:North American Aviation 1364:RD-250 to 252, 261, 262 292:hypergolic fuel mixture 1938:Spacecraft components 1840:are under development 1228:YF-20, 21, 22, 24, 25 1007:RD-107, 108, 117, 118 1329:RD-0216, 0217, 0235 992:RD-0107, 0108, 0110 267:Pressure-fed engine 21: 1918:Rocketdyne engines 351:ballistic missiles 323:. Rocket engineer 95:Liquid-fuel engine 1875: 1874: 1847: 1846: 1789:Space Shuttle SRB 1530: 1529: 1468: 1467: 1158: 1157: 880: 879: 317:vernier thrusters 259:vernier thrusters 225: 224: 209:Rated for 184 Sec 155:Thrust, sea-level 40:Country of origin 1955: 1896: 1889: 1882: 1858: 1851: 1538: 1537: 1374:RD-263, 268, 273 1305:along other LREs 1167: 1027:RD-191, 151, 181 891: 549: 540: 494: 487: 480: 471: 459: 458: 456: 455: 446:. Archived from 440: 434: 433: 431: 430: 421:. Archived from 415: 409: 408: 406: 405: 396:. Archived from 390: 296:Triethylaluminum 273:corrections and 229:vernier thruster 189:Specific impulse 80:Vernier Thruster 29: 22: 1963: 1962: 1958: 1957: 1956: 1954: 1953: 1952: 1903: 1902: 1901: 1900: 1848: 1843: 1825: 1546: 1539: 1535: 1526: 1464: 1354:RD-0255 to 0257 1349:RD-0243 to 0245 1211: 1200: 1196: 1190: 1178: 1154: 895: 886: 876: 740: 734: 728: 559: 553: 534: 527: 514: 512:launch vehicles 498: 468: 463: 462: 453: 451: 442: 441: 437: 428: 426: 417: 416: 412: 403: 401: 392: 391: 387: 382: 363: 336:RP-2 (Kerosene) 325:Robert C. Truax 313: 283: 248:launch vehicles 35: 33:Robert C. 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1309: 1304: 1303:Paektusan LRE 1301: 1300: 1298: 1294: 1291: 1290: 1288: 1284: 1281: 1279: 1276: 1275: 1273: 1269: 1266: 1264: 1261: 1259: 1256: 1254: 1251: 1250: 1248: 1244: 1241: 1239: 1236: 1234: 1231: 1229: 1226: 1224: 1221: 1220: 1218: 1217: 1215: 1212: 1205: 1201: 1189: 1185: 1181: 1176: 1172: 1168: 1165: 1161: 1149: 1146: 1144: 1141: 1139: 1136: 1134: 1131: 1129: 1126: 1124: 1121: 1119: 1116: 1114: 1111: 1109: 1106: 1104: 1101: 1099: 1096: 1094: 1091: 1089: 1086: 1084: 1081: 1080: 1078: 1074: 1073: 1069: 1067: 1066: 1062: 1060: 1057: 1056: 1054: 1050: 1047: 1046: 1044: 1040: 1037: 1035: 1034: 1030: 1028: 1025: 1023: 1020: 1018: 1015: 1013: 1010: 1008: 1005: 1003: 1000: 998: 995: 993: 990: 988: 987:RD-0105, 0109 985: 983: 980: 978: 975: 973: 970: 969: 967: 963: 962: 958: 957: 955: 951: 950: 946: 944: 943: 939: 937: 934: 932: 929: 927: 924: 922: 921: 917: 915: 912: 911: 909: 908: 906: 903: 899: 892: 889: 883: 871: 870: 866: 864: 863: 859: 858: 856: 852: 851: 847: 846: 844: 840: 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264: 260: 256: 251: 249: 246: 242: 238: 234: 231:developed by 230: 221: 217: 212: 208: 204: 198: 195: 193: 190: 186: 180: 177: 175: 173: 168: 162: 159: 157: 153: 149: 145: 140: 136: 132: 129:Configuration 127: 124: 120: 119:Gas Generator 117: 113: 110: 106: 103: 99: 96: 92: 88: 84: 81: 78: 74: 71: 68: 64: 61: 58: 54: 50: 46: 43:United States 42: 38: 34: 28: 23: 1868:expanding it 1861: 1837: 1378: 1299:North Korea 1070: 1063: 1031: 959: 947: 940: 918: 867: 860: 848: 836: 829: 822: 800: 793: 786: 769: 762: 755: 699: 692: 680: 658: 601: 594: 505:solid motors 452:. Retrieved 448:the original 438: 427:. Retrieved 423:the original 413: 402:. Retrieved 398:the original 388: 333: 314: 294:composed of 284: 252: 250:until 1990. 226: 123:Pressure-fed 66:Manufacturer 20:LR-101-NA-11 1836:Engines in 1483:RD-109, 119 1421:RD-864, 869 1406:RD-854, 861 1369:RD-253, 275 1017:RD-170, 171 367:SM-65 Atlas 348:PGM-17 Thor 344:SM-65 Atlas 329:PGM-17 Thor 220:PGM-17 Thor 191:, sea-level 142:Performance 76:Application 1907:Categories 1223:YF-1, 2, 3 1171:Hypergolic 1143:Rutherford 862:Prometheus 824:Archimedes 454:2020-12-25 429:2020-12-24 404:2020-12-24 380:References 373:Rocketdyne 271:trajectory 263:turbopumps 233:Rocketdyne 101:Propellant 70:Rocketdyne 60:Rocketdyne 1764:Castor 30 1644:Zefiro 40 1639:Zefiro 23 1580:SpaB-140C 977:NK-33, 44 887:cryogenic 733:Methalox 552:Hydrolox 544:Cryogenic 357:rockets. 206:Burn time 1779:Orbus-21 1634:Zefiro 9 1397:Ukraine 1175:Aerozine 1163:Storable 1055:Ukraine 997:RD-0110R 894:Kerolox 361:See also 281:Variants 172:pressure 170:Chamber 56:Designer 1838:italics 1799:Star 48 1794:Star 37 1774:Orbus-6 1695:Israel 1629:Waxwing 1585:Europe 1577:SpaB-65 1479:Russia 1344:RD-0237 1339:RD-0236 1310:Russia 1289:Israel 1249:Europe 1093:Kestrel 1039:S1.5400 1002:RD-0124 968:Russia 961:SCE-200 857:Europe 850:RD-0169 845:Russia 771:Longyun 764:Lingyun 682:RD-0146 676:RD-0120 667:Russia 624:Vulcain 610:Europe 533:Liquid 509:orbital 214:Used in 134:Chamber 89:Retired 1754:AJ-60A 1719:KM-V2b 1710:Japan 1684:Salman 1650:India 1624:Topaze 1589:Mage 1 1554:China 1545:Solid 1452:TR-201 1416:RD-856 1411:RD-855 1401:RD-843 1391:S5.98M 1380:RD-270 1274:India 1268:Viking 1258:Astris 1253:Aestus 1243:YF-50D 1219:China 1128:RS-27A 1118:Merlin 1108:LR-105 1072:RD-810 1065:RD-801 1049:TEPREL 1045:Spain 1033:RD-193 1022:RD-180 1012:RD-120 956:India 949:Welkin 942:YF-130 936:YF-115 931:YF-102 926:YF-100 910:China 838:Aeon R 831:Aeon 1 818:Raptor 802:YF-215 795:YF-209 788:TQ-15A 752:China 645:Japan 634:CE-7.5 630:India 585:YF-75D 571:China 86:Status 1819:X-254 1814:X-248 1804:UA120 1784:Orion 1759:Algol 1744:SRB-A 1739:M-34c 1714:KM-V1 1704:RSA-3 1680:Iran 1573:FG-47 1568:FG-46 1563:FG-36 1558:FG-02 1519:XLR81 1513:RS-88 1508:Curie 1498:Gamma 1473:Other 1457:XLR81 1446:RS-88 1441:LR-91 1436:LR-87 1386:S5.92 1314:17D61 1283:Vikas 1263:Vexin 1238:YF-40 1233:YF-23 1206:, or 1186:, or 1180:UH 25 1148:XLR50 1133:RS-56 1123:RS-27 1103:LR-89 1098:LR-79 982:RD-58 972:NK-15 920:TH-12 914:TH-11 885:Semi- 782:TQ-12 777:TQ-11 757:BF-20 722:RS-68 717:RS-25 694:BE-3U 639:CE-20 619:Vinci 603:YF-90 596:YF-79 590:YF-77 580:YF-75 575:YF-73 355:Delta 245:Delta 237:Atlas 115:Cycle 1864:stub 1809:SRMU 1734:M-34 1729:M-24 1724:M-14 1699:LK-1 1689:Rafe 1674:S200 1669:S139 1619:P230 1614:P120 1547:fuel 1431:AJ10 1293:LK-4 1188:UDMH 1138:S-3D 1059:RD-8 898:RP-1 869:M-10 813:BE-4 712:RL10 701:BE-7 660:LE-9 654:LE-7 649:LE-5 614:HM7B 535:fuel 507:for 503:and 346:and 340:RP-1 298:and 243:and 241:Thor 109:RP-1 51:1958 48:Date 1769:GEM 1664:S12 1609:P80 1604:PAP 1599:P-6 1594:P-4 1494:UK 1278:PS4 1208:HNO 1204:MON 1184:MMH 1088:H-1 1083:F-1 902:LOX 744:LOX 707:J-2 563:LOX 105:LOX 1909:: 1659:S9 1654:S7 1202:, 1191:/ 1182:, 1177:, 900:/ 742:/ 737:CH 561:/ 556:LH 239:, 121:/ 107:/ 1895:e 1888:t 1881:v 1870:. 1521:* 1515:* 1459:* 1448:* 1213:) 1210:3 1199:4 1197:O 1195:2 1193:N 1173:( 904:) 896:( 746:) 739:4 735:( 565:) 558:2 554:( 493:e 486:t 479:v 457:. 432:. 407:. 137:1

Index


Robert C. Truax
Rocketdyne
Rocketdyne
Vernier Thruster
Liquid-fuel engine
LOX
RP-1
Gas Generator
Pressure-fed
pressure
Specific impulse
PGM-17 Thor
vernier thruster
Rocketdyne
Atlas
Thor
Delta
launch vehicles
yaw, pitch and roll control
vernier thrusters
turbopumps
Pressure-fed engine
trajectory
stabilization
pyrotechnical ignition system
hypergolic fuel mixture
Triethylaluminum
Triethylborane
gimbal mounts

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