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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
620:
would have consisted of a S-IC C-4B first stage, a S-II C-5A second stage and a S-IVB C-5A third stage. It would have been capable of sending a 31,000 kg (68,000 lb) payload to a translunar trajectory.
915:
739:
David S. Akens, Saturn
Illustrated Chronology: Saturn's First Eleven Years, April 1957 through April 1968, 5th ed., MHR-5 (Huntsville, AL : MSFC, 20 Jan. 1971).
567:
C series studied from 1959 to 1962. The C-4 design was proposed in 1960 for a three-stage launch vehicle that could launch 99,000 kg (218,000 lb) to
2649:
Symbol indicates past or current rockets that attempted orbital launches but never succeeded (never did or has yet to perform a successful orbital launch)
705:
613:
eventually used the lunar orbit rendezvous method to go to the Moon, it decided to use the larger Saturn V which would provide a reserve payload capacity.
780:
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NASA, "Earth
Orbital Rendezvous for an Early Manned Lunar Landing," pt. I, "Summary Report of Ad Hoc Task Group Study" , August 1961.
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Stuhlinger, Ernst, et al., Astronautical
Engineering and Science: From Peenemuende to Planetary Space, McGraw-Hill, New York, 1964.
353:
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third stage. The first and second stages were essentially four-engine variants of the stages that would be used on the
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into lunar orbit, but it would not have been able to carry the 15,000 kg (32,000 lb)
576:
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2186:
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1257:
572:
178:
730:. Excellent account of the evolution, design, and development of the Saturn launch vehicles.
586:
It would have consisted of three stages; an S-IB-4 first stage, a S-II-4 second stage and a
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8:
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722:
Bilstein, Roger E, Stages to Saturn, US Government
Printing Office, 1980.
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It would have been capable of sending the 30,000 kg (67,000 lb)
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594:, while the IVB stage was actually used on both the Saturn V and the
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and send 32,000 kg (70,000 lb) to the Moon via
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687:. 2012-06-17. Archived from the original on 2012-06-17
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704:: CS1 maint: bot: original URL status unknown (
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754:National Aeronautics and Space Administration
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25:
575:. It met the initial requirements for a
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16:Proposed NASA super-heavy-lift rocket
806:Comparison of orbital launch systems
718:Encyclopedia Astronautica Saturn C-4
679:
677:
636:List of space launch system designs
315:6,000,000 lbf (27,000 kN)
293:1,599,433 lb (725,491 kg)
143:1,023,670 lb (464,330 kg)
13:
752:from websites or documents of the
14:
3041:
674:
658:. Astronautix.com. Archived from
484:271,000 lb (123,000 kg)
387:449,840 lb (204,040 kg)
2727:
748: This article incorporates
743:
503:225,000 lbf (1,000 kN)
409:800,000 lbf (3,600 kN)
285:149,945 lb (68,014 kg)
172:218,000 lb (99,000 kg)
3025:Cancelled space launch vehicles
2634:Super heavy-lift launch vehicle
616:A December 1961 version called
476:29,700 lb (13,500 kg)
379:54,978 lb (24,938 kg)
188:70,000 lb (32,000 kg)
801:List of orbital launch systems
648:
1:
641:
603:Apollo Command/Service Module
563:was the fourth rocket in the
269:113.10 ft (34.47 m)
2690:Saturn launch vehicle family
513:421 seconds (4.13 km/s)
363:69.80 ft (21.28 m)
7:
624:
521:165 + 335 seconds (2 burns)
127:269.0 ft (82.0 m)
10:
3046:
2624:Medium-lift launch vehicle
460:61.6 ft (18.8 m)
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2629:Heavy-lift launch vehicle
2619:Small-lift launch vehicle
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468:21.7 ft (6.6 m)
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371:320 in (8.1 m)
277:320 in (8.1 m)
135:320 in (8.1 m)
790:Orbital launch systems
750:public domain material
577:lunar orbit rendezvous
573:trans-lunar injection
248:Kennedy Space Center
609:as well. Although
607:Apollo Lunar Module
419:300 sec (sea level)
325:265 sec (sea level)
21:
1796:v1.2 "Full Thrust"
197:Associated rockets
31:Saturn C-4B on pad
19:
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95:Country of origin
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2882:Saturn II series
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2505:Universal Rocket
876:Falcon 9 Block 5
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550:edit on Wikidata
509:Specific impulse
415:Specific impulse
321:Specific impulse
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2697:Early proposals
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662:on 17 June 2012
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569:low Earth orbit
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352:Second stage –
230:Proposed (1962)
103:Cost per launch
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494:Rocketdyne J-2
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449:Third stage –
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312:Maximum thrust
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258:First stage –
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222:Launch history
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71:North American
68:
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38:
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15:
9:
6:
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3:
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2510:UR-500 Proton
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886:Firefly Alpha
884:
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738:
735:
732:
729:
728:0-16-048909-1
725:
721:
719:
716:
715:
707:
701:
686:
685:"Saturn C-4B"
680:
678:
661:
657:
651:
647:
637:
634:
632:
629:
628:
622:
619:
614:
612:
608:
604:
599:
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589:
584:
582:
581:lunar landing
578:
574:
570:
566:
562:
551:
545:
541:
538:
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516:
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398:
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264:
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256:
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171:
167:
164:
159:
154:
150:
146:
142:
138:
134:
130:
126:
122:
117:
113:
111:Cost per year
109:
105:
101:
98:United States
97:
93:
86:
82:
79:
76:
72:
69:
66:
62:
59:
58:
56:
52:
49:
46:
42:
39:
35:
28:
23:
2941:
2919:
2800:
2793:
2765:
2760:
2743:
2404:Thorad-Agena
2077:Soyuz/Vostok
881:Falcon Heavy
742:
689:. Retrieved
664:. Retrieved
660:the original
656:"Saturn C-4"
650:
617:
615:
600:
585:
560:
558:
235:Launch sites
106:43.5 million
54:Manufacturer
1894:LauncherOne
1845:Kaituozhe-1
1622:Black Arrow
1374:Orbex Prime
1273:Hyperbola-2
1238:Antares 330
938:Kaituozhe 2
911:Hyperbola-1
618:Saturn C-4B
427:200 seconds
333:139 seconds
177:Payload to
161:Payload to
3014:Categories
2969:Saturn V-3
2745:Saturn C-1
2737:"C" series
2709:Saturn A-1
1899:Long March
1803:Feng Bao 1
1416:Tianlong-3
1342:New Line 1
1300:Long March
1248:Cyclone-4M
1188:Tianlong-2
1166:2.1b / STB
1161:2.1a / STA
1104:Pegasus XL
970:Long March
943:Kinetica 1
866:Chollima-1
691:2023-12-26
642:References
631:Saturn C-3
561:Saturn C-4
526:Propellant
489:Powered by
481:Gross mass
473:Empty mass
432:Propellant
397:Rocketdyne
392:Powered by
384:Gross mass
376:Empty mass
338:Propellant
303:Rocketdyne
298:Powered by
290:Gross mass
282:Empty mass
212:Comparable
20:Saturn C-4
2994:V-Centaur
2889:Saturn II
1998:Paektusan
1627:Conestoga
1384:Red Dwarf
1337:New Glenn
1268:Gravity-2
1258:Epsilon S
891:Gravity-1
596:Saturn IB
583:mission.
518:Burn time
424:Burn time
330:Burn time
156:Capacity
3030:Saturn C
2921:Saturn V
2795:Saturn I
2542:original
2532:Vanguard
2515:Proton-K
2488:original
2336:Ablestar
2321:Terran 1
2279:original
2138:Rocket 3
2045:original
1855:original
1781:Falcon 9
1776:Falcon 1
1732:IV Heavy
1448:Zuljanah
1411:Terran R
1394:Block 1B
1379:Pallas-1
1283:Kuaizhou
1243:Bloostar
1183:Starship
1134:Shavit 2
1119:Qaem 100
1109:Proton-M
1067:Minotaur
948:Kuaizhou
871:Electron
839:Ariane 6
700:cite web
625:See also
592:Saturn V
465:Diameter
368:Diameter
274:Diameter
238:planned
216:Saturn V
132:Diameter
37:Function
2607:Classes
2478:Tsyklon
2316:Start-1
2087:Voskhod
2082:Sputnik
2018:Molniya
2003:Pilot-2
1840:Juno II
1754:Epsilon
1749:Energia
1739:Diamant
1615:Centaur
1464:Antares
1457:Retired
1406:Soyuz-7
1399:Block 2
1332:Neutron
1322:Miura 5
1156:Soyuz-2
1149:Block 1
1139:Simorgh
916:Jielong
844:Atlas V
815:Current
81:Douglas
2999:Jarvis
2959:INT-25
2954:INT-24
2949:INT-23
2943:INT-21
2937:INT-20
2904:INT-19
2899:INT-18
2894:INT-17
2868:INT-27
2863:INT-16
2858:INT-15
2853:INT-14
2848:INT-13
2843:INT-12
2838:INT-11
2833:INT-05
2704:Juno V
2591:Zhuque
2525:Strela
2483:R-36-O
2426:II GLV
2414:SLV-2H
2409:SLV-2G
2397:DSV-2U
2375:Burner
2311:SS-520
2306:Sparta
2274:Shavit
2165:Saturn
2126:Shtil'
2092:Vostok
2035:Polyot
1993:Naro-1
1882:Lambda
1850:Kosmos
1835:Juno I
1759:Europa
1533:Athena
1496:Ariane
1436:Zhuque
1426:Vega E
1278:Irtysh
1215:Zhuque
933:KAIROS
822:Angara
726:
666:8 June
565:Saturn
457:Height
360:Height
354:S-II-4
266:Height
260:S-IB-4
240:SLC 37
227:Status
206:Saturn
202:Family
148:Stages
124:Height
61:Boeing
2932:V ELV
2808:IB-CE
2554:Zenit
2549:VLS-1
2520:Rokot
2421:Titan
2392:Delta
2353:Agena
2301:SPARK
2187:Scout
2143:Safir
2131:Volna
2040:Soyuz
1830:H-IIB
1744:Dnepr
1632:Delta
1610:Agena
1600:SLV-3
1595:LV-3B
1550:Atlas
1124:Qased
1099:OS-M1
901:H-IIA
849:Ceres
588:S-IVB
548:[
451:S-IVB
244:LC-39
45:Lunar
2828:IB-D
2823:IB-C
2818:IB-B
2813:IB-A
2773:C-5N
2579:3SLB
2537:Vega
2466:CT-3
2451:IIIE
2446:IIID
2441:IIIC
2436:IIIB
2431:IIIA
2331:Able
2326:Thor
2227:X-2B
2217:X-3M
2207:X-2M
2121:R-29
2013:Luna
1988:N-II
1966:3SII
1865:2/2I
1825:H-II
1813:Mk I
1808:GSLV
1791:v1.1
1786:v1.0
1712:5000
1707:4000
1702:3000
1697:2000
1692:1000
1687:0100
1605:Able
1528:ASLV
1489:230+
1431:Zero
1357:OS-M
1352:Nova
1347:NGLV
1263:Eris
1253:Deca
1198:Vega
1193:Unha
1178:SSLV
1171:2-1v
1114:PSLV
1094:Nuri
1062:LVM3
995:3B/E
896:GSLV
724:ISBN
706:link
668:2012
611:NASA
579:and
559:The
342:RP-1
185:Mass
169:Mass
140:Mass
119:Size
114:1985
85:S-IV
75:S-II
65:S-IB
43:and
2989:V-D
2984:V-C
2979:V-B
2974:V-A
2927:MLV
2873:LCB
2778:C-8
2767:C-5
2761:C-4
2756:C-3
2751:C-2
2719:B-1
2714:A-2
2574:3SL
2569:2FG
2461:23G
2456:34D
2291:SLV
2267:G-1
2262:F-1
2257:E-1
2252:A-1
2247:D-1
2242:B-1
2222:X-4
2212:X-3
2202:X-2
2192:X-1
2008:R-7
1983:N-I
1820:H-I
1722:III
1590:III
1565:E/F
1484:230
1479:130
1474:120
1469:110
1421:VLM
1389:SLS
1327:MLV
1144:SLS
1129:RS1
1055:11H
827:1.2
537:LOX
443:LOX
400:J-2
346:LOX
306:F-1
179:TLI
163:LEO
41:LEO
3016::
2802:IB
2584:3F
2564:2M
2471:IV
2175:IB
2158:1B
2153:1A
2112:2M
2070:U2
2050:FG
1978:N1
1961:3S
1956:3H
1951:3C
1946:4S
1941:Mu
1934:4A
1929:3B
1919:2E
1914:2A
1909:1D
1887:4S
1875:3M
1769:II
1727:IV
1717:II
1585:II
1543:II
1315:12
1310:10
1293:31
1288:21
1077:IV
1050:11
1040:7A
1030:6A
1020:5B
1010:4C
1005:4B
1000:3C
990:3A
985:2F
980:2D
975:2C
963:11
958:1A
906:H3
859:1S
832:A5
756:.
702:}}
698:{{
676:^
598:.
535:/
530:LH
492:1
441:/
436:LH
395:4
301:4
246:;
242:,
2682:e
2675:t
2668:v
2596:1
2559:2
2498:3
2493:2
2385:2
2380:1
2368:D
2363:B
2358:A
2346:2
2341:1
2284:1
2237:A
2232:B
2180:V
2170:I
2148:1
2107:2
2102:K
2097:L
2065:U
2060:M
2055:L
2028:L
2023:M
1971:V
1924:3
1904:1
1870:3
1860:1
1764:I
1682:N
1677:M
1672:L
1667:J
1662:G
1657:E
1652:D
1647:C
1642:B
1637:A
1580:I
1575:H
1570:G
1560:D
1555:B
1538:I
1521:5
1516:4
1511:3
1506:2
1501:1
1441:3
1367:4
1362:2
1305:9
1220:2
1203:C
1087:C
1082:V
1072:I
1045:8
1035:7
1025:6
1015:5
953:1
926:3
921:1
854:1
782:e
775:t
768:v
708:)
694:.
670:.
552:]
532:2
438:2
344:/
151:3
87:)
83:(
77:)
73:(
67:)
63:(
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