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Jupiter-C

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The upper-stage tub was visibly spun-up before launch. During first-stage flight, the vehicle was guided by a gyro-controlled autopilot controlling both air-vanes and jet vanes on the first stage by means of servos. Following a vertical launch from a simple steel table, the vehicle was programmed so
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project, and the sequence of manufacture of the rockets (which are not necessarily launched in order, and may be uprated as solutions to technical problems are worked out in tests) was considered a military secret. So the designation painted on the sides of the rocket was not a serial number in
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fired and springs separated the instrument section from the first-stage tankage. The instrument section and the spinning tub were slowly tipped to a horizontal position by means of four air jets located at the base of the instrument section. When the apex of the vertical flight occurred after a
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shaft mounted on the first-stage instrument section. Two electric motors spun in the tub at a rate varying from 450 to 750 rpm to compensate for thrust imbalance when the clustered motors fired. The rate of spin was varied by a programmer so that it did not couple with the changing resonance
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with two solid-propellant upper stages. The tanks of the Redstone were lengthened by 8 ft (2.4 m) to provide additional propellant. The instrument compartment was also smaller and lighter than the Redstone's. The second and third stages were clustered in a "tub" atop the vehicle.
638:. Since the Juno I was the same height as the Jupiter-C (21.2 meters), with the added fourth stage being hidden inside the shell, this vehicle which successfully launched the first orbital satellite of the United States is often incorrectly referred to as a Jupiter-C. 629:
was a satellite launch vehicle based on the Jupiter-C, but with the addition of a fourth stage, atop the "tub" of the third stage and the use of Hydyne as fuel. The Juno name derived from Von Braun wishing to make the satellite launch appear as peaceable as the
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rocket engines; the third stage was a cluster of three scaled-down Sergeant rockets grouped within. These were held in position by bulkheads and rings and surrounded by a cylindrical outer shell. The webbed base plate of the shell rested on a
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coasting flight of about 247 seconds, a radio signal from the ground ignited the eleven-rocket cluster of the second stage, separating the tub from the instrument section. The third stage then fired to raise the
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This Template lists historical, current, and future space rockets that at least once attempted (but not necessarily succeeded in) an orbital launch or that are planned to attempt such a launch in the future
805:: Jupiter-C RS-40, lifted a 1/3-scale Jupiter nose cone to an altitude of 285 mi (460 km) and a range of 1,330 mi (2,140 km); Juno I (four-stage configuration). 799:: Jupiter-C RS-34, lifted a 300 lb (140 kg) scale Jupiter ablative nose cone to an altitude of 350 mi (560 km) and a range of 710 mi (1,100 km). 1244: 659:, giving HUNTSVILE, with duplicated letters dropped: H was used for 1, U for 2, ..., E for 9 and X for 0. For example, the Jupiter-C / Juno I modified to launch 2978:
Symbol indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)
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mobile missile. The recovered nosecone was displayed in the Oval Office as part of President Dwight D. Eisenhower's televised speech on November 7, 1957.
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that it was traveling at an angle of 40 degrees from the horizontal at burnout of the first stage, which occurred 157 seconds after launch.
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Yanek Mieczkowski, 'Cheerleader in Chief, in Eisenhower’s Sputnik Moment: The Race for Space and World Prestige, pp. 105–106.
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Juno V Space Vehicle Development Program Status Report, DSP-TM-11-58, NASA, November, 1958.
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Juno V Space Vehicle Development Program Report No. DSP-TM-10-58, NASA, October, 1958.
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turbopump drive, 90% hydrogen peroxide decomposed by catalyst bed to produce steam
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Overall, takeoff: 64,000 lb (29,000 kg)/10,230 lb (4640 kg)
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Stage 1 62,700 lb (28,400 kg)/9,600 lb (4,400 kg)
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was an American research and development vehicle developed from the
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had "UE" painted on the side, indicating it was S/N 29 (U→2, E→9).
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Stage 2 1,020 lb (460 kg)/490 lb (220 kg)
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propellants, liquid oxygen, as oxidizer, and alcohol as fuel
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propellant, polysulfide-aluminum and ammonium perchlorate (
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Stage 3 280 lb (130 kg)/140 lb (64 kg)
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The second stage was an outer ring of eleven scaled-down
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that were later to be deployed on the more advanced
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Unsourced material may be challenged and removed. 339:93,560 lbf; 416.18 kN (42,439 kgf) 2989: 823:"Redstone Arsenal Historical Information – 1957" 399:16,500 lbf; 73.4 kN (7,480 kgf) 328:1 North American Aviation (Rocketdyne) 75-110- 1103: 1016:"Rockets and Missiles / Jupiter C Fact Sheet" 445:2,040 kgf (4,500 lbf; 20.0 kN) 1063: 1061: 1059: 587:frequency of the first stage during flight. 765:specific impulse, 235 s (2.30 kN·s/kg) 740:specific impulse, 220 s (2.16 kN·s/kg) 709:specific impulse, 235 s (2.30 kN·s/kg) 3008:Space launch vehicles of the United States 1117: 1110: 1096: 666: 641: 127: 1056: 907: 905: 903: 901: 109:Learn how and when to remove this message 568: 549: 2990: 898: 3003:Sounding rockets of the United States 1091: 703:Thrust, 83,000 lbf (370 kN) 542:Each vehicle consisted of a modified 514:, Jupiter-C was designed by the U.S. 258:Cape Canaveral Missile Annex, Florida 1135:Comparison of orbital launch systems 954:. United States Army. Archived from 929:. United States Army. Archived from 850:. United States Army. Archived from 825:. United States Army. Archived from 734:Thrust, 16,500 lbf (73 kN) 47:adding citations to reliable sources 18: 759:Thrust, 4,500 lbf (24 kN) 603:. Through this system, designed by 13: 16:Part of the Redstone rocket family 14: 3019: 776: 530:article). All were launched from 23: 2963:Super heavy-lift launch vehicle 1040:"SP-4402 Origins of NASA Names" 1032: 1008: 999: 768:propellant, same as for Stage 2 752:Stage 3: Three JPL scaled-down 715:propellant feed, turbopump type 518:(ABMA), under the direction of 492:. Jupiter-C was used for three 133:Jupiter-C on the launch pad at 34:needs additional citations for 1130:List of orbital launch systems 990: 969: 944: 919: 889: 865: 840: 815: 646:The Jupiter-C was part of the 537: 195:64,000 pounds (29,000 kg) 1: 809: 516:Army Ballistic Missile Agency 7: 523: 455:214 s (2.10 km/s) 409:214 s (2.10 km/s) 349:235 s (2.30 km/s) 10: 3024: 2953:Medium-lift launch vehicle 618: 544:Redstone ballistic missile 2971: 2958:Heavy-lift launch vehicle 2948:Small-lift launch vehicle 2935: 1785: 1559: 1143: 1125: 979:. Designation-systems.net 672:Weight as configured for 614: 607:in 1956 for his proposed 499:in 1956 and 1957 to test 471: 467: 459: 449: 441: 430: 421: 413: 403: 395: 384: 375: 361: 353: 343: 335: 324: 315: 311: 303: 295: 287: 279: 271: 263: 245: 237: 232: 228: 220: 212: 207: 199: 191: 183: 175: 170: 162: 151: 141: 126: 594:At first-stage burnout, 497:sub-orbital spaceflights 667:General characteristics 642:Encrypted serial number 532:Cape Canaveral, Florida 224:11 kg (24 lb) 179:69.9 feet (21.3 m) 1119:Orbital launch systems 913:"Jupiter-C Explorer-I" 873:"Rockets and Missiles" 574: 566: 512:Redstone rocket family 676:launch, loaded/empty 572: 553: 187:5.8 feet (1.8 m) 573:Second stage cluster 43:improve this article 2998:1956 in spaceflight 1073:Gunter's Space Page 762:burning time, 6.5 s 737:burning time, 6.5 s 706:burning time, 155 s 657:Huntsville, Alabama 123: 2125:v1.2 "Full Thrust" 783:September 20, 1956 575: 567: 501:re-entry nosecones 299:September 20, 1956 288:Partial failure(s) 267:3 (all suborbital) 121: 2985: 2984: 1020:www.spaceline.org 605:Wernher von Braun 520:Wernher von Braun 482: 481: 163:Country of origin 119: 118: 111: 93: 3015: 2834:Universal Rocket 1205:Falcon 9 Block 5 1112: 1105: 1098: 1089: 1088: 1083: 1082: 1080: 1079: 1065: 1054: 1053: 1051: 1050: 1044:history.nasa.gov 1036: 1030: 1029: 1027: 1026: 1012: 1006: 1003: 997: 994: 988: 987: 985: 984: 973: 967: 966: 964: 963: 948: 942: 941: 939: 938: 923: 917: 916: 909: 896: 893: 887: 886: 884: 883: 869: 863: 862: 860: 859: 844: 838: 837: 835: 834: 819: 745:solid propellant 723:Stage 2: Eleven 565:rockets compared 563:Mercury-Redstone 510:A member of the 475:edit on Wikidata 451:Specific impulse 405:Specific impulse 345:Specific impulse 131: 124: 120: 114: 107: 103: 100: 94: 92: 51: 27: 19: 3023: 3022: 3018: 3017: 3016: 3014: 3013: 3012: 2988: 2987: 2986: 2981: 2967: 2943:Sounding rocket 2931: 1781: 1555: 1139: 1121: 1116: 1086: 1077: 1075: 1067: 1066: 1057: 1048: 1046: 1038: 1037: 1033: 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1011: 1002: 993: 978: 977:"ABMA Juno I" 972: 958:on 2015-07-03 957: 953: 947: 933:on 2015-05-18 932: 928: 922: 914: 908: 906: 904: 902: 892: 878: 877:SpaceLine.org 874: 868: 854:on 2015-05-18 853: 849: 843: 829:on 2015-05-18 828: 824: 818: 814: 804: 801: 798: 795: 792: 788: 784: 781: 780: 767: 764: 761: 758: 757: 755: 754:Baby Sergeant 751: 746: 742: 739: 736: 733: 732: 730: 729:Baby Sergeant 726: 722: 717: 714: 711: 708: 705: 702: 701: 699: 695: 694: 692: 687: 684: 681: 678: 677: 675: 671: 670: 664: 662: 658: 654: 649: 639: 637: 633: 628: 622: 612: 610: 606: 602: 597: 592: 588: 585: 580: 571: 564: 560: 556: 552: 548: 545: 535: 533: 529: 526:below or the 525: 521: 517: 513: 508: 506: 502: 498: 495: 491: 487: 476: 470: 466: 462: 458: 454: 452: 448: 444: 440: 437: 433: 429: 425: 420: 416: 412: 408: 406: 402: 398: 394: 391: 387: 383: 379: 374: 371: 367: 364: 360: 356: 352: 348: 346: 342: 338: 334: 331: 327: 323: 319: 314: 310: 306: 302: 298: 294: 290: 286: 282: 278: 274: 270: 266: 262: 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Retrieved 1072: 1047:. Retrieved 1043: 1034: 1023:. Retrieved 1019: 1010: 1001: 992: 981:. Retrieved 971: 960:. Retrieved 956:the original 946: 935:. Retrieved 931:the original 921: 891: 880:. Retrieved 876: 867: 856:. Retrieved 852:the original 842: 831:. Retrieved 827:the original 817: 802: 797:May 15, 1957 796: 782: 727:scaled-down 645: 624: 593: 589: 584:ball bearing 576: 558: 541: 509: 485: 483: 296:First flight 246:Launch sites 158:for the ABMA 152:Manufacturer 105: 99:October 2007 96: 86: 79: 72: 65: 53: 41:Please help 36:verification 33: 2223:LauncherOne 2174:Kaituozhe-1 1951:Black Arrow 1703:Orbex Prime 1602:Hyperbola-2 1567:Antares 330 1267:Kaituozhe 2 1240:Hyperbola-1 1069:"Jupiter-C" 700:A-7 engine 693:Propulsion 538:Description 320:(stretched) 304:Last flight 272:Success(es) 215:Sub-orbital 213:Payload to 58:"Jupiter-C" 2992:Categories 2228:Long March 2132:Feng Bao 1 1745:Tianlong-3 1671:New Line 1 1629:Long March 1577:Cyclone-4M 1517:Tianlong-2 1495:2.1b / STB 1490:2.1a / STA 1433:Pegasus XL 1299:Long March 1272:Kinetica 1 1195:Chollima-1 1078:2023-10-14 1049:2018-12-26 1025:2018-04-19 983:2013-03-25 962:2015-05-15 937:2015-05-15 882:2018-04-19 858:2015-05-15 833:2015-05-15 810:References 793:, Florida. 698:Rocketdyne 674:Explorer 1 661:Explorer 1 653:clear text 431:Powered by 385:Powered by 362:Propellant 325:Powered by 280:Failure(s) 69:newspapers 2327:Paektusan 1956:Conestoga 1713:Red Dwarf 1666:New Glenn 1597:Gravity-2 1587:Epsilon S 1220:Gravity-1 787:satellite 696:Stage 1: 559:Jupiter-C 490:Jupiter-A 486:Jupiter-C 460:Burn time 414:Burn time 354:Burn time 208:Capacity 122:Jupiter-C 2871:original 2861:Vanguard 2844:Proton-K 2817:original 2665:Ablestar 2650:Terran 1 2608:original 2467:Rocket 3 2374:original 2184:original 2110:Falcon 9 2105:Falcon 1 2061:IV Heavy 1777:Zuljanah 1740:Terran R 1723:Block 1B 1708:Pallas-1 1612:Kuaizhou 1572:Bloostar 1512:Starship 1463:Shavit 2 1448:Qaem 100 1438:Proton-M 1396:Minotaur 1277:Kuaizhou 1200:Electron 1168:Ariane 6 756:rockets 731:rockets 579:Sergeant 555:Redstone 494:uncrewed 424:Sergeant 378:Sergeant 318:Redstone 184:Diameter 156:Chrysler 142:Function 2936:Classes 2807:Tsyklon 2645:Start-1 2416:Voskhod 2411:Sputnik 2347:Molniya 2332:Pilot-2 2169:Juno II 2083:Epsilon 2078:Energia 2068:Diamant 1944:Centaur 1793:Antares 1786:Retired 1735:Soyuz-7 1728:Block 2 1661:Neutron 1651:Miura 5 1485:Soyuz-2 1478:Block 1 1468:Simorgh 1245:Jielong 1173:Atlas V 1144:Current 915:. NASA. 426:cluster 380:cluster 241:Retired 83:scholar 2920:Zhuque 2854:Strela 2812:R-36-O 2755:II GLV 2743:SLV-2H 2738:SLV-2G 2726:DSV-2U 2704:Burner 2640:SS-520 2635:Sparta 2603:Shavit 2494:Saturn 2455:Shtil' 2421:Vostok 2364:Polyot 2322:Naro-1 2211:Lambda 2179:Kosmos 2164:Juno I 2088:Europa 1862:Athena 1825:Ariane 1765:Zhuque 1755:Vega E 1607:Irtysh 1544:Zhuque 1262:KAIROS 1151:Angara 636:Viking 627:Juno I 621:Juno I 615:Juno I 601:apogee 528:Juno I 524:Juno I 370:Hydyne 238:Status 200:Stages 176:Height 85:  78:  71:  64:  56:  2883:Zenit 2878:VLS-1 2849:Rokot 2750:Titan 2721:Delta 2682:Agena 2630:SPARK 2516:Scout 2472:Safir 2460:Volna 2369:Soyuz 2159:H-IIB 2073:Dnepr 1961:Delta 1939:Agena 1929:SLV-3 1924:LV-3B 1879:Atlas 1453:Qased 1428:OS-M1 1230:H-IIA 1178:Ceres 473:[ 436:Solid 390:Solid 357:155 s 90:JSTOR 76:books 2908:3SLB 2866:Vega 2795:CT-3 2780:IIIE 2775:IIID 2770:IIIC 2765:IIIB 2760:IIIA 2660:Able 2655:Thor 2556:X-2B 2546:X-3M 2536:X-2M 2450:R-29 2342:Luna 2317:N-II 2295:3SII 2194:2/2I 2154:H-II 2142:Mk I 2137:GSLV 2120:v1.1 2115:v1.0 2041:5000 2036:4000 2031:3000 2026:2000 2021:1000 2016:0100 1934:Able 1857:ASLV 1818:230+ 1760:Zero 1686:OS-M 1681:Nova 1676:NGLV 1592:Eris 1582:Deca 1527:Vega 1522:Unha 1507:SSLV 1500:2-1v 1443:PSLV 1423:Nuri 1391:LVM3 1324:3B/E 1225:GSLV 648:IRBM 625:The 561:and 484:The 252:and 250:LC-5 221:Mass 192:Mass 171:Size 62:news 2903:3SL 2898:2FG 2790:23G 2785:34D 2620:SLV 2596:G-1 2591:F-1 2586:E-1 2581:A-1 2576:D-1 2571:B-1 2551:X-4 2541:X-3 2531:X-2 2521:X-1 2337:R-7 2312:N-I 2149:H-I 2051:III 1919:III 1894:E/F 1813:230 1808:130 1803:120 1798:110 1750:VLM 1718:SLS 1656:MLV 1473:SLS 1458:RS1 1384:11H 1156:1.2 725:JPL 463:6 s 417:6 s 388:11 366:LOX 330:A-7 45:by 2994:: 2913:3F 2893:2M 2800:IV 2504:IB 2487:1B 2482:1A 2441:2M 2399:U2 2379:FG 2307:N1 2290:3S 2285:3H 2280:3C 2275:4S 2270:Mu 2263:4A 2258:3B 2248:2E 2243:2A 2238:1D 2216:4S 2204:3M 2098:II 2056:IV 2046:II 1914:II 1872:II 1644:12 1639:10 1622:31 1617:21 1406:IV 1379:11 1369:7A 1359:6A 1349:5B 1339:4C 1334:4B 1329:3C 1319:3A 1314:2F 1309:2D 1304:2C 1292:11 1287:1A 1235:H3 1188:1S 1161:A5 1071:. 1058:^ 1042:. 1018:. 900:^ 875:. 557:, 534:. 434:3 256:, 2925:1 2888:2 2827:3 2822:2 2714:2 2709:1 2697:D 2692:B 2687:A 2675:2 2670:1 2613:1 2566:A 2561:B 2509:V 2499:I 2477:1 2436:2 2431:K 2426:L 2394:U 2389:M 2384:L 2357:L 2352:M 2300:V 2253:3 2233:1 2199:3 2189:1 2093:I 2011:N 2006:M 2001:L 1996:J 1991:G 1986:E 1981:D 1976:C 1971:B 1966:A 1909:I 1904:H 1899:G 1889:D 1884:B 1867:I 1850:5 1845:4 1840:3 1835:2 1830:1 1770:3 1696:4 1691:2 1634:9 1549:2 1532:C 1416:C 1411:V 1401:I 1374:8 1364:7 1354:6 1344:5 1282:1 1255:3 1250:1 1183:1 1111:e 1104:t 1097:v 1081:. 1052:. 1028:. 986:. 965:. 940:. 885:. 861:. 836:. 747:) 477:] 368:/ 254:6 203:3 112:) 106:( 101:) 97:( 87:· 80:· 73:· 66:· 39:.

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Cape Canaveral
Sounding rocket
Chrysler
Sub-orbital
LC-5
6
Cape Canaveral Missile Annex, Florida
Redstone
A-7
Specific impulse
LOX
Hydyne
Sergeant
Solid
Specific impulse
Sergeant
Solid
Specific impulse

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