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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.
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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).
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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
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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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655:, but employed a simple transformation cypher that the staff would be sure not to forget. The key was taken from the name of the design and test base:
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789:) to an altitude of 680 mi (1,100 km), a speed of 16,000 mph (7 km/s), and a range of 3,300 mi (5,300 km) from
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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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522:. Three Jupiter-C flights were made. These were followed by satellite launches with the vehicle designated as Juno I (see
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785:: Jupiter-C RS-27, lifted an 86.5-lb (39.2 kg) payload (including a 30-lb (14 kg) dummy
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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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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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propellants, liquid oxygen, as oxidizer, and alcohol as fuel
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927:"Redstone Arsenal Historical Information – Redstone Rocket"
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propellant, polysulfide-aluminum and ammonium perchlorate (
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The second stage was an outer ring of eleven scaled-down
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952:"Redstone Arsenal Historical Information – Explorer I"
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that were later to be deployed on the more advanced
848:"Redstone Arsenal Historical Information – Jupiter"
49:. Unsourced material may be challenged and removed.
339:93,560 lbf; 416.18 kN (42,439 kgf)
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823:"Redstone Arsenal Historical Information – 1957"
399:16,500 lbf; 73.4 kN (7,480 kgf)
328:1 North American Aviation (Rocketdyne) 75-110-
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1016:"Rockets and Missiles / Jupiter C Fact Sheet"
445:2,040 kgf (4,500 lbf; 20.0 kN)
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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
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109:Learn how and when to remove this message
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3003:Sounding rockets of the United States
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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
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759:Thrust, 4,500 lbf (24 kN)
603:. Through this system, designed by
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16:Part of the Redstone rocket family
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530:article). All were launched from
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2963:Super heavy-lift launch vehicle
1040:"SP-4402 Origins of NASA Names"
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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
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349:235 s (2.30 km/s)
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979:. Designation-systems.net
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667:General characteristics
642:Encrypted serial number
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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"
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676:launch, loaded/empty
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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
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2125:v1.2 "Full Thrust"
783:September 20, 1956
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299:September 20, 1956
288:Partial failure(s)
267:3 (all suborbital)
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1020:www.spaceline.org
605:Wernher von Braun
520:Wernher von Braun
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1215:Firefly Alpha
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978:
977:"ABMA Juno I"
972:
958:on 2015-07-03
957:
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947:
933:on 2015-05-18
932:
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877:SpaceLine.org
874:
868:
854:on 2015-05-18
853:
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829:on 2015-05-18
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754:Baby Sergeant
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729:Baby Sergeant
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526:below or the
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166:United States
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67:
63:
60: –
59:
55:
54:Find sources:
48:
44:
38:
37:
32:This article
30:
26:
21:
20:
2733:Thorad-Agena
2406:Soyuz/Vostok
1210:Falcon Heavy
1076:. 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
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