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UA120

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1757: 1380: 17: 55: 75:(LITVC) system, with an external nacelle containing nitrogen tetroxide attached to the side of each booster. Solid fueled separation rockets, used to jettison the spent boosters, were affixed at the top and bottom of the stage. Thrust-termination capability, necessary for crewed rockets such as the 62:
All versions of UA120 shared a common design, with the only significant differentiating factor being the length of the motor. It was a segmented design, with between five and seven motor segments possible. A solid propellant used was a
83:, was to be provided by two pyrotechnically triggered ports on the forward closure, which when opened would allow for the non-propulsive venting of exhaust gasses. The forward end of the stage contained an aerodynamic 1982: 95:
The overall design of each variant was very similar, the main difference being the number of segments used. This is indicated by the number at the end of each designation.
1959: 1954: 1517: 1949: 1944: 1939: 1934: 87:, an ignitor, separation rockets, and the forward attachment ring. The aft end contained additional separation rockets, the nozzle, and a heat shield. 1890: 1512: 1865: 1977: 1895: 1885: 1880: 1875: 71:(PBAN) binder. The stage had an external diameter of 120 inches. Attitude control in flight was provided by means of a liquid injection 2162: 2157: 1870: 64: 1507: 1502: 1497: 1121: 335: 1715: 1997: 1992: 265: 366: 291: 175: 2013: 1632: 1987: 2038: 1926: 1031: 313: 1662: 213:"A STUDY OF PERFORMANCE AND COST IMPROVEMENT POTENTIAL OF THE 120-IN.- (3.05 M) DIAMETER SOLID ROCKET MOTOR" 2018: 328: 2260: 1708: 68: 240: 212: 2090: 2048: 1652: 986: 705: 667: 80: 1969: 951: 946: 2043: 2028: 1047: 376: 941: 2204: 1388: 614: 607: 467: 321: 2111: 1746: 1701: 1472: 1341: 1111: 1101: 792: 774: 1013: 1736: 1657: 1607: 1527: 1487: 1482: 1477: 1351: 1126: 1076: 1014: 462: 1532: 2126: 2116: 2033: 2023: 1839: 1627: 1622: 1617: 1612: 1602: 1036: 348: 132: 35: 681: 674: 8: 1756: 1637: 1457: 1157: 1027: 712: 352: 43: 2230: 1452: 1783: 1582: 1562: 72: 2209: 2152: 1778: 981: 399: 269: 39: 295: 179: 1860: 956: 936: 931: 926: 550: 387: 355: 343: 2254: 961: 745: 661: 587: 406: 344: 152: 147:. It was proposed for several other variants of Titan III and IV, as well as 76: 32: 1799: 148: 16: 2106: 1741: 1051: 1018: 1677:* Different versions of the engine use different propellant combinations 1467: 1900: 1824: 1819: 1814: 1809: 1804: 1106: 116: 112: 108: 104: 2131: 1834: 1829: 1442: 1437: 1086: 128: 84: 21: 1844: 1547: 1542: 1462: 1447: 1432: 1136: 840: 144: 2235: 2225: 2121: 1905: 1642: 1197: 1192: 1187: 1182: 1177: 1172: 1167: 1162: 882: 845: 835: 830: 804: 693: 580: 525: 519: 54: 1693: 46:). Several variants existed, with a varying number of segments. 1597: 1331: 1326: 1295: 1264: 1259: 1254: 1249: 1244: 1234: 1223: 1217: 1212: 1207: 1202: 1146: 1096: 971: 915: 908: 892: 876: 870: 865: 860: 855: 850: 785: 779: 769: 645: 638: 477: 428: 2172: 2167: 2147: 1587: 1416: 1411: 1406: 1401: 1362: 1356: 1300: 1289: 1279: 1229: 1081: 1071: 1023: 991: 976: 966: 825: 820: 815: 763: 757: 631: 625: 620: 600: 565: 560: 537: 514: 482: 446: 439: 433: 423: 418: 2177: 1284: 1274: 1066: 902: 741: 656: 555: 544: 503: 497: 492: 457: 241:"Study of Solid Rocket Motors for a Space Shuttle Booster" 1577: 1572: 1567: 1557: 737: 170: 168: 38:, manufactured by the Chemical Systems Division of 235: 233: 207: 205: 203: 201: 199: 197: 2252: 165: 230: 194: 1709: 329: 127:The UA1206 was used as a strap-on booster on 115:rockets, and was proposed for use on several 103:UA1205 was used as a strap-on booster on the 218:. United Aircraft Corporation. December 1971 1716: 1702: 336: 322: 246:. United Technology Center. 15 March 1972 65:ammonium perchlorate composite propellant 53: 15: 149:derivatives of the Saturn rocket family 117:derivatives of the Saturn rocket family 2253: 1697: 317: 367:Comparison of orbital rocket engines 13: 14: 2272: 1723: 1755: 1378: 44:United Technologies Corporation 284: 258: 58:Schematic of the UA120 booster 1: 1163:RD-0202 to 0206, 0208 to 0213 294:. Astronautix. Archived from 268:. Astronautix. Archived from 178:. Astronautix. Archived from 158: 7: 90: 69:polybutadiene acrylonitrile 10: 2277: 81:Manned Orbiting Laboratory 2218: 2197: 2190: 2140: 2099: 2068: 2061: 2006: 1968: 1925: 1918: 1853: 1792: 1771: 1764: 1753: 1729: 1673: 1387: 1376: 1316: 1006: 728: 576: 395: 386: 375: 362: 138: 122: 98: 49: 24:with two UA1206 boosters 1208:RD-250 to 252, 261, 262 59: 25: 1684:are under development 1072:YF-20, 21, 22, 24, 25 851:RD-107, 108, 117, 118 73:thrust vector control 57: 36:solid rocket boosters 19: 1840:Commercial Titan III 133:Commercial Titan III 2231:Pratt & Whitney 1173:RD-0216, 0217, 0235 836:RD-0107, 0108, 0110 272:on February 8, 2002 143:UA1207 was used on 2261:Solid-fuel rockets 60: 26: 2248: 2247: 2244: 2243: 2186: 2185: 2057: 2056: 1914: 1913: 1691: 1690: 1633:Space Shuttle SRB 1374: 1373: 1312: 1311: 1002: 1001: 724: 723: 2268: 2195: 2194: 2066: 2065: 1923: 1922: 1784:LGM-25C Titan II 1769: 1768: 1759: 1718: 1711: 1704: 1695: 1694: 1382: 1381: 1218:RD-263, 268, 273 1149:along other LREs 1011: 1010: 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articles 1728: 1724:Titan rockets 1719: 1714: 1712: 1707: 1705: 1700: 1699: 1696: 1683: 1679: 1676: 1675: 1672: 1664: 1661: 1659: 1656: 1654: 1651: 1649: 1646: 1644: 1641: 1639: 1636: 1634: 1631: 1629: 1626: 1624: 1621: 1619: 1616: 1614: 1611: 1609: 1606: 1604: 1601: 1599: 1596: 1595: 1593: 1589: 1586: 1584: 1581: 1579: 1576: 1574: 1571: 1569: 1566: 1564: 1561: 1559: 1556: 1555: 1553: 1549: 1546: 1544: 1541: 1540: 1538: 1534: 1531: 1529: 1526: 1525: 1523: 1519: 1516: 1514: 1511: 1509: 1506: 1504: 1501: 1499: 1496: 1495: 1493: 1489: 1486: 1484: 1481: 1479: 1476: 1474: 1471: 1469: 1466: 1464: 1461: 1459: 1456: 1454: 1451: 1449: 1446: 1444: 1441: 1439: 1436: 1434: 1431: 1430: 1428: 1423: 1420: 1418: 1415: 1413: 1410: 1408: 1405: 1403: 1400: 1399: 1397: 1396: 1394: 1392: 1386: 1364: 1361: 1358: 1355: 1353: 1350: 1349: 1347: 1343: 1340: 1339: 1337: 1333: 1332:RD-211 to 214 1330: 1328: 1325: 1324: 1322: 1321: 1319: 1315: 1302: 1299: 1297: 1294: 1291: 1288: 1286: 1283: 1281: 1278: 1276: 1273: 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Retrieved 296:the original 286: 274:. Retrieved 270:the original 260: 248:. Retrieved 220:. Retrieved 184:. Retrieved 180:the original 142: 126: 102: 94: 61: 28: 27: 20:Launch of a 2049:Little Rock 1742:SM-68 Titan 1680:Engines in 1327:RD-109, 119 1265:RD-864, 869 1250:RD-854, 861 1213:RD-253, 275 861:RD-170, 171 302:26 February 276:26 February 250:26 February 222:26 February 186:26 February 2062:Components 1970:Vandenberg 1901:Titan IIIM 1896:Titan IIIL 1825:Titan IIIE 1820:Titan IIID 1815:Titan IIIC 1810:Titan IIIB 1805:Titan IIIA 1067:YF-1, 2, 3 1015:Hypergolic 987:Rutherford 706:Prometheus 668:Archimedes 159:References 145:Titan IV-A 113:Titan IIIE 109:Titan IIID 105:Titan IIIC 2132:Transtage 2044:McConnell 2029:Ellsworth 1886:Titan IIS 1881:Titan IIL 1876:Titan IIB 1835:Titan 23G 1830:Titan 34D 1608:Castor 30 1488:Zefiro 40 1483:Zefiro 23 1424:SpaB-140C 821:NK-33, 44 731:cryogenic 577:Methalox 396:Hydrolox 388:Cryogenic 129:Titan 34D 85:nose cone 22:Titan 34D 2255:Category 2163:Orbus 21 2069:Boosters 1960:(S)LC-41 1955:(S)LC-40 1845:Titan IV 1772:Missiles 1747:Launches 1623:Orbus-21 1478:Zefiro 9 1241:Ukraine 1019:Aerozine 1007:Storable 899:Ukraine 841:RD-0110R 738:Kerolox 292:"UA1207" 176:"UA1205" 151:and the 91:Variants 33:American 2236:Thiokol 2226:Aerojet 2219:Engines 2158:Orbus 6 2141:Engines 2122:Star-37 2112:Centaur 1906:Titan V 1871:Titan-C 1854:Unbuilt 1765:Rockets 1682:italics 1643:Star 48 1638:Star 37 1618:Orbus-6 1539:Israel 1473:Waxwing 1429:Europe 1421:SpaB-65 1323:Russia 1188:RD-0237 1183:RD-0236 1154:Russia 1133:Israel 1093:Europe 937:Kestrel 883:S1.5400 846:RD-0124 812:Russia 805:SCE-200 701:Europe 694:RD-0169 689:Russia 615:Longyun 608:Lingyun 526:RD-0146 520:RD-0120 511:Russia 468:Vulcain 454:Europe 377:Liquid 353:orbital 42:(later 2205:Martin 2198:Rocket 2153:B-8096 2086:UA1207 2081:UA1206 2076:UA1205 2014:Larson 1988:LC-395 1891:Soltan 1598:AJ-60A 1563:KM-V2b 1554:Japan 1528:Salman 1494:India 1468:Topaze 1433:Mage 1 1398:China 1389:Solid 1296:TR-201 1260:RD-856 1255:RD-855 1245:RD-843 1235:S5.98M 1224:RD-270 1118:India 1112:Viking 1102:Astris 1097:Aestus 1087:YF-50D 1063:China 972:RS-27A 962:Merlin 952:LR-105 916:RD-810 909:RD-801 893:TEPREL 889:Spain 877:RD-193 866:RD-180 856:RD-120 800:India 793:Welkin 786:YF-130 780:YF-115 775:YF-102 770:YF-100 754:China 682:Aeon R 675:Aeon 1 662:Raptor 646:YF-215 639:YF-209 632:TQ-15A 596:China 489:Japan 478:CE-7.5 474:India 429:YF-75D 415:China 139:UA1207 123:UA1206 111:, and 99:UA1205 50:Design 2173:LR-91 2168:LR-87 2148:AJ-10 2107:Agena 2034:Lowry 2024:Beale 2007:Bases 1998:SLC-6 1993:SLC-4 1950:LC-20 1945:LC-19 1940:LC-16 1935:LC-15 1663:X-254 1658:X-248 1648:UA120 1628:Orion 1603:Algol 1588:SRB-A 1583:M-34c 1558:KM-V1 1548:RSA-3 1524:Iran 1417:FG-47 1412:FG-46 1407:FG-36 1402:FG-02 1363:XLR81 1357:RS-88 1352:Curie 1342:Gamma 1317:Other 1301:XLR81 1290:RS-88 1285:LR-91 1280:LR-87 1230:S5.92 1158:17D61 1127:Vikas 1107:Vexin 1082:YF-40 1077:YF-23 1050:, or 1030:, or 1024:UH 25 992:XLR50 977:RS-56 967:RS-27 947:LR-89 942:LR-79 826:RD-58 816:NK-15 764:TH-12 758:TH-11 729:Semi- 626:TQ-12 621:TQ-11 601:BF-20 566:RS-68 561:RS-25 538:BE-3U 483:CE-20 463:Vinci 447:YF-90 440:YF-79 434:YF-77 424:YF-75 419:YF-73 244:(PDF) 216:(PDF) 67:with 29:UA120 2178:RL10 2091:SRMU 1983:SLTF 1978:OSTF 1861:Ares 1653:SRMU 1578:M-34 1573:M-24 1568:M-14 1543:LK-1 1533:Rafe 1518:S200 1513:S139 1463:P230 1458:P120 1391:fuel 1275:AJ10 1137:LK-4 1032:UDMH 982:S-3D 903:RD-8 742:RP-1 713:M-10 657:BE-4 556:RL10 545:BE-7 504:LE-9 498:LE-7 493:LE-5 458:HM7B 379:fuel 351:for 347:and 304:2016 278:2016 252:2016 224:2016 188:2016 131:and 2127:TOS 2117:IUS 1613:GEM 1508:S12 1453:P80 1448:PAP 1443:P-6 1438:P-4 1338:UK 1122:PS4 1052:HNO 1048:MON 1028:MMH 932:H-1 927:F-1 746:LOX 588:LOX 551:J-2 407:LOX 79:or 2257:: 1503:S9 1498:S7 1046:, 1035:/ 1026:, 1021:, 744:/ 586:/ 581:CH 405:/ 400:LH 232:^ 196:^ 167:^ 155:. 135:. 119:. 107:, 1717:e 1710:t 1703:v 1365:* 1359:* 1303:* 1292:* 1057:) 1054:3 1043:4 1041:O 1039:2 1037:N 1017:( 748:) 740:( 590:) 583:4 579:( 409:) 402:2 398:( 337:e 330:t 323:v 306:. 280:. 254:. 226:. 190:.

Index


Titan 34D
American
solid rocket boosters
United Aircraft
United Technologies Corporation

ammonium perchlorate composite propellant
polybutadiene acrylonitrile
thrust vector control
Space Shuttle
Manned Orbiting Laboratory
nose cone
Titan IIIC
Titan IIID
Titan IIIE
derivatives of the Saturn rocket family
Titan 34D
Commercial Titan III
Titan IV-A
derivatives of the Saturn rocket family
Space Shuttle


"UA1205"
the original



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