View source for PGM-19 Jupiter

{{more footnotes needed|date=November 2020}}
{{Use dmy dates|date=April 2017}}
{{Infobox weapon
|is_missile      = yes
|name            = SM-78/PGM-19 Jupiter
|image           = Jupiter emplacement.jpg
|image_size      = 300
|caption         = Jupiter missile emplacement showing ground support equipment. The bottom third of the missile is encased in a "flower petal shelter" of wedge-shaped metal panels allowing crews to service the missile in all weather conditions.
|origin          = United States
|type            = [[Medium-range ballistic missile]] (MRBM)
|service         =
|used_by         = {{unbulleted list
  | [[United States Air Force]]
  | [[Italian Air Force]]
  | [[Turkish Air Force]]
  }}
|wars            =
<!-- Production history -->
|designer        =
|design_date     = 1954
|manufacturer    = Chrysler
|unit_cost       =
|production_date = 1956–1961
|number          = approx. 100 (45 deployed)
|variants        = Juno II
<!-- General specifications -->
|spec_label      =
|weight          = {{cvt|110,000|lb|kg}}
|length          = {{cvt|60|ft|m|1}}
|part_length     =
|width           =
|height          =
|diameter        = {{cvt|8|ft|9|in|m|2}}
|crew            =
|passengers      =
<!-- Explosive specifications --> 
| filling            = {{unbulleted list
  | [[W38 (nuclear warhead)|W38]] (3.75 Mt){{citation needed|date=August 2025}}
  | [[W49]] (1.44 Mt)
  }}
| filling_weight     = 
| detonation         = 
| yield              =  {{unbulleted list
  | 3.75 Mt
  | 1.44 Mt
  }}
<!-- Vehicle/missile specifications -->
| primary_armament   = [[W38 (nuclear warhead)|W38 warhead]] 3.75 Mt or [[W49]] 1.44 Mt
| engine             =  Rocketdyne LR79-NA (Model S-3D) liquid LRE
| engine_power       = {{cvt|150,000|lbf|kN}}
<!-- Missiles only -->
|wingspan        =
|propellant      = kerosene and liquid oxygen
|ceiling         = {{cvt|380|mi|km}}
|altitude        =
|depth           =
|boost           =
|launch_platform =
|transport       = 
|vehicle_range   = {{cvt|1,500-1,700|miles|km}}
}}

The '''PGM-19 Jupiter''' was the first [[nuclear weapon|nuclear armed]], [[medium-range ballistic missile]] (MRBM) of the [[United States Air Force]] (USAF). It was a [[liquid-propellant rocket]] using [[RP-1]] fuel and [[Liquid oxygen|LOX]] oxidizer, with a single [[Rocketdyne S-3D|Rocketdyne LR79-NA]] (model S-3D) [[rocket engine]] producing {{cvt|150,000|lbf|kN}} of thrust. It was armed with the {{cvt|1.44|MtonTNT}} [[W49]] nuclear warhead. The prime contractor was the [[Chrysler Corporation]].

The Jupiter was originally designed by the [[US Army]], which was looking for a highly accurate missile designed to strike enemy states such as [[China]] and the [[Soviet Union]]. The [[US Navy]] also expressed an interest in the design as an [[SLBM]] but left the collaboration to work on their solid-fuel [[UGM-27 Polaris|Polaris]]. Jupiter retained the short, squat shape intended to fit in submarines.

==Development history==

===Initial concept===
Jupiter traces its history ultimately to the [[PGM-11 Redstone]] missile, the US's first nuclear ballistic missile. While it was entering service, [[Wernher von Braun]]'s [[Army Ballistic Missile Agency]] (ABMA) team at [[Redstone Arsenal]] began to consider an upgraded version using the LR89 rocket engine being developed by [[Rocketdyne]] for the Air Force's [[Atlas missile]] project. Using the LR89 and adding a second stage would allow the new design to reach {{convert|1000|nmi}},{{sfn|Kyle|2011|loc=IRBM Battle}} a dramatic improvement over the Redstone's roughly {{convert|200|miles}}.

As Rocketdyne continued working on the LR89, it appeared that it could be improved to increase thrust over the promised {{convert|120000|lbf}}. In 1954, the Army asked Rocketdyne to provide a similar design with a thrust of {{convert|135000|lbf}}.{{sfn|Healy|1958|p=1}} During this same period, the weight of nuclear warheads was rapidly falling, and by combining this engine with a warhead of {{convert|2000|lbs}} they could build a single-stage missile able to reach {{convert|1500-1700|miles}} while being significantly less complicated and easier to handle in the field than a two-stage model. This engine was continually upgraded, ultimately reaching {{convert|150000|lbf}}.{{sfn|Kyle|2011|loc=IRBM Battle}} This last model, known to the Army as the NAA-150-200, became much better known by its Rocketdyne model number, S-3.{{sfn|Kyle|2011|loc=The Design}}

===Navy SLBM interest===
[[File:Arleigh Burke 1951.jpg|thumb|right|Admiral Arleigh Burke is credited with breaking the Navy out of its moribund ways, and pressing for development of the SLBM.]]

Around the same time, the [[US Navy]] was looking for ways to join the nuclear club, and had been focusing mostly on [[cruise missile]]s and similar systems. Some consideration had been given to the use of ballistic missiles on ships, but Admiral [[Hyman Rickover]], "father" of the nuclear submarine, was skeptical that this could be done, and was worried it would take up funding needed elsewhere.{{sfn|Mackenzie|1993|p=135}} Another skeptic of missiles was the [[Chief of Naval Operations]], [[Robert B. Carney]].{{sfn|Mackenzie|1993|p=136}}

Lower-ranking Navy officials became increasingly interested when the Army and Air Force began serious development of their long-range missiles. In an attempt to bypass high-ranking Navy officials, who remained uninterested in the concept, the Navy liaison to the [[Killian Committee]] championed the cause. The Committee took up the concept, and in September 1955 released a report calling for the development of a sea-based missile system.{{sfn|Mackenzie|1993|p=136}}

The Navy's interest in missiles had been greatly increased with the August 1955 appointment of Admiral [[Arleigh Burke]] to replace Carney. Burke was convinced the Navy had to get into the missile field as rapidly as possible, and was well aware that the Air Force would oppose any such endeavor. Instead, he approached the Army, and found that the proposed Jupiter fit the range goals needed by the Navy.{{sfn|Mackenzie|1993|p=136}}

===Development begins===
The issue of who would be given the go-ahead to build an [[IRBM]] by this time had reached the [[Joint Chiefs of Staff]] (JCS), who proved unable to reach a decision. This forced the Secretary of Defense [[Charles Erwin Wilson]] to move ahead without an official recommendation from the military. He saw the Navy interest as a reasonable argument to continue the Army project in any event, and on 8 November 1955 approved both programs. The Air Force would develop IRBM No. 1, or SM-75 (for "strategic missile"), the Army would develop their design as IRBM No. 2 or {{nowrap|SM-78}}. The Navy would develop systems to launch the Army missile from ships and, later, submarines.{{sfn|Mackenzie|1993|p=136}}{{sfn|Neufeld|1990|p=121}} [[BuShips]] completed a conceptual design that would take a [[United States Maritime Administration|Maritime Administration]] {{nowrap|[[Type C4-class ship|type C4-S-1a]]}} hull and convert it into a Jupiter missile launch ship, which was given the [[hull classification symbol|hull symbols]] [[List of yard and district craft of the United States Navy#District Auxiliary, Miscellaneous (YAG)|YAG-58]] then [[List of auxiliaries of the United States Navy#Miscellaneous Ships (AG, T-AG)|EAG-155]]; the conversion would later be canceled.<ref>{{cite web |url=https://www.shipscribe.com/usnaux2/AG/AG155.html |title=Class: Unnamed (EAG 155, C4-S-1a) }}</ref>

The requirement for shipboard storage and launching dictated the size and shape of the Jupiter. The original Army design was {{convert|92|feet}} long and {{convert|95|inch}} in diameter. The Navy stated they were not interested in anything longer than {{convert|50|feet}}. The ABMA team responded by increasing the diameter to {{convert|105|inch}}. This precluded it from being carried aboard contemporary [[cargo aircraft]], limiting it to sea and road. Even with this change, they were unable to reduce its length enough to suit the Navy. They suggested that they begin with a {{convert|60|foot}} long version and then scale it down as improvements in the engines were worked into the design. This was rejected, and after briefly considering a {{convert|55|foot}} version, finally settled on the {{convert|58|foot}} version.{{sfn|Kyle|2011|loc=Defining the Army/Navy Jupiter}}

On 2 December 1955, the secretaries of the Army and Navy publicly announced the dual Army–Navy program to create a land- and sea-based MRBM. In April 1956, as part of a widespread effort to assign names to various missile projects, the Army's effort was given the name "Jupiter" and the Air Force's became "Thor".{{sfn|Kyle|2011|loc=IRBM Battle}}

===Accuracy and mission===
Redstone provided an accuracy of {{convert|300|m|order=flip}} at its maximum range, which, when combined with its large warhead, allowed it to attack hard targets like protected airbases, bridges, command and control sites, as well as other strategic targets like railway marshaling yards and pre-attack concentration areas. This was in keeping with the Army's view of nuclear weapons, which was in effect more powerful [[artillery]]. They saw the weapons as part of a large-scale battle in Europe, in which both sides would use nuclear weapons during a limited war that did not include the use of strategic weapons on each other's cities. In that case, "if wars were to be kept limited, such weapons would have to be capable of hitting only tactical targets." This approach saw the support of a number of influential theorists, notably [[Henry Kissinger]], and was seized on as a uniquely Army mission.{{sfn|Mackenzie|1993|p=132}}

The original goal for the new longer-range design was to match Redstone's accuracy at the Jupiter's much-extended range. That is, if Redstone could reach {{cvt|300|m|order=flip}} at {{cvt|200|miles}}, the new design would provide a [[circular error probable]] on the order of {{convert|7|km|order=flip}}. As development continued, it became clear the ABMA team, under the direction of [[Fritz Mueller]], could improve on that. This led to a period in which "The Army would lay down a particular accuracy, and wait for our arguments whether it was possible. We had to promise a lot, but were fortunate."{{sfn|Mackenzie|1993|p=131}}

This process ultimately delivered a superior design intended to provide {{convert|0.5|mile}} accuracy at the full range, an order of magnitude better than Redstone and four times better than the best INS designs being used by the Air Force. The system was so accurate that a number of observers expressed their skepticism about the Army's goals, with the [[Weapons Systems Evaluation Group|WSEG]] suggesting they were hopelessly optimistic.{{sfn|Mackenzie|1993|p=131}}

The Air Force was dead set against Jupiter. They argued that nuclear weapons were not simply new artillery, and that their employment would immediately trigger a response that might result in a strategic exchange. This would especially be true if the Army launched a long-range weapon like Jupiter, which could reach cities in the Soviet Union and could not immediately be distinguished as attacking a military or civilian target. They suggested that any such launch would trigger a strategic response, and as such, the Army should not be given any long-range weapons.{{sfn|Mackenzie|1993|p=131}}

However, as von Braun's team went from success to success, and with Atlas still years from operational deployment, it was clear that Jupiter represented a threat to the Air Force's desired hegemony over strategic forces. This led to them starting their own MRBM program [[PGM-17 Thor|Thor]], in spite of having repeatedly dismissed the medium-range role in the past.{{sfn|Mackenzie|1993|p= 120}} The fighting between the Army and Air Force grew through 1955 and 1956 until practically every missile system the Army was involved in was being attacked in the press.<ref>{{cite news |title=Air Force Calls Army Unfit to Guard Nation |newspaper=New York Times |date=21 May 1956 |page=1}}</ref>

===Navy exit===
[[File:Polaris A3 (A3X-01) on pad LC-29A at CCSFS - 1962-08-07.jpg|thumb|right|The Navy's Polaris had range similar to Jupiter.]]

The Navy was concerned from the start about Jupiter's [[cryogenic propellant]]s, but at the time there was no other option. Given the size and weight of contemporary nuclear weapons, only a large liquid-fuel rocket engine provided the energy needed to meet the Navy's range goal of launching from safe areas in the Atlantic Ocean. They justified the risk thus:

{{cquote|We were prepared to take the chance that we might lose a submarine or two through accidental explosions. But, then, there are some of us who enjoy, or at lease &#91;sic&#93; are acclimated to, the idea of risking our lives."{{sfn|Mackenzie|1993|p=137}}}}

All of this changed radically in the summer of 1956, when [[Project Nobska]] brought together leading scientists to consider antisubmarine warfare. As part of this workshop, [[Edward Teller]] stated that by 1963 a 1&nbsp;megaton warhead would be reduced to only {{convert|600|lbs}}.<ref>{{cite book |first=Elliot |last=Converse III |title= Rearming for the Cold War 1945 – 1960 |url=https://history.defense.gov/Portals/70/Documents/acquisition_pub/OSDHO-Acquisition-Series-Vol1.pdf |page=527 |publisher= Government Printing Office |date= 2012}}</ref> Rocketry experts at the same meeting suggested that an intermediate-range weapon carrying one of these weapons could be built using [[solid propellant]]. Even in this case, the missile would be much smaller than Jupiter; Jupiter was expected to weigh {{convert|160000|lb}}, while estimates of a solid-fuel missile with similar range were closer to {{convert|30000|lb}}, along with a similar reduction in size which was of paramount importance to a submarine design.{{sfn|Mackenzie|1993|p=138}}

The Navy announced their desire to develop their own missile that summer, initially under the name Jupiter-S. After intensive follow-up studies, the Navy withdrew from the Jupiter program in December 1956. This was officially announced by the Army in January 1957.<ref>{{cite web |url=https://history.redstone.army.mil/ihist-1957.html |title=Installation history, 1957 |website=US Army Redstone Arsenal History}}</ref> In its place, the Navy began development of what was then known as the Fleet Ballistic Missile Program, and the missile was later renamed [[UGM-27 Polaris|Polaris]], their first [[submarine-launched ballistic missile]] (SLBM).<ref>{{Cite journal|jstor=resrep12035.7|title=The U.S. Navy's Fleet Ballistic Missile Program and Finite Deterrence|last1=Sapolsky|first1=Harvey M.|journal=Getting Mad|year=2004|pages=123–136}}</ref> Rickover, one of the few remaining skeptics, was won over by pointing out that a properly designed submarine was needed specifically for this role, and he would be called upon to produce it. Rickover was from that point on a staunch ally of the program.{{sfn|Mackenzie|1993|p=139}}

===Saved from cancellation===
[[File:McElroy at ABMA.jpg|thumb|right|Secretary of Defence Neil McElroy visits the Jupiter prototype assembly line at ABMA. ABMA built the test articles, while Chrysler built the production models.]]

On 4 October 1957, the Soviets successfully launched [[Sputnik I]] from their [[R-7 Semyorka]] ICBM. The US was aware of these efforts and had already talked to the press about it, suggesting that if the Soviets launched a satellite first it would be no big deal.<ref>{{cite news | url=https://archive.org/stream/galaxymagazine-1958-11/Galaxy_1958_11#page/n47/mode/2up | title=How Secret was Sputnik No. 1? | work=Galaxy | date=November 1958 | access-date=13 June 2014 | author=Ley, Willy | pages=48–50}}</ref> To their surprise, the press exploded in rage over the affair. Having spent over a decade working on similar missiles, like [[Atlas ICBM|Atlas]], the fact that the Soviets could beat them was a serious blow, and prompted a deep review of the ongoing programs.<ref>{{cite news|last=David |first=Leonard |title=Sputnik 1: The Satellite That Started It All |work=Space.com |date=4 October 2002 |url=http://www.space.com/missionlaunches/sputnik_45th_anniversary_021004.html |access-date=20 January 2007 |url-status=dead |archive-url=https://web.archive.org/web/20060216013800/http://www.space.com/missionlaunches/sputnik_45th_anniversary_021004.html |archive-date=16 February 2006 }}</ref>

One problem noted from the start was that the internecine fighting between the Army and Air Force was leading to significant duplication of effort, with little to show for it. The Department of Defense responded by creating the Advanced Research Projects Agency ([[DARPA|ARPA]]), whose initial mission was to look over all of the ongoing projects and select ones based solely on their technical merits.{{sfn|Kyle|2011|loc=Air Force Gains Control}}

At the same time, the fighting had begun to have negative political effects. In a 26 November 1956 memorandum, recently appointed [[US Secretary of Defense]] [[Charles Erwin Wilson]] attempted to end the fighting. His solution was to limit the Army to weapons with {{convert|200|mi|adj=on}} range, and those involved in surface-to-air defense to only {{convert|100|mi}}.<ref name=larsen>{{cite news |first=Douglas |last=Larsen |url=https://news.google.com/newspapers?nid=1798&dat=19570801&id=DuIiAAAAIBAJ&pg=7135,197246 |access-date=18 May 2013 |title=New Battle Looms Over Army's Newest Missile |newspaper=Sarasota Journal |date=1 August 1957 |page=35}}</ref> The memo also placed limits on Army air operations, severely limiting the weight of the aircraft it was allowed to operate. To some degree this simply formalized what had largely already been the case in practice, but Jupiter fell outside the range limits and the Army was forced to hand them to the Air Force.<ref>{{cite book |last= Trest |first= Warren |title= Air Force Roles and Missions: A History |url=https://books.google.com/books?id=R4xOJW8EBwAC&pg=PA175 |publisher= Government Printing Office |year= 2010 |isbn= 9780160869303 |page=175}}</ref>

The Air Force, of course, had no interest in taking over a weapon system they had long argued was not needed. However, ARPA's studies clearly showed it was an excellent system, and as it was ready to enter production, any Air Force thoughts about canceling it were immediately quashed. New orders for 32 prototypes and 62 operational missiles were soon placed, bringing the total number of Jupiters to be built to 94. The first, hand-built at ABMA, would be delivered by the end of FY57, and the first production models from Chrysler's Michigan Ordnance Missile Plant near [[Warren, Michigan]] between FY58 and FY61.{{sfn|Kyle|2011|loc=Air Force Gains Control}}

===Lingering complaints===
A primary complaint about Jupiter was that the design's shorter range placed it within relatively easy striking distance of Soviet weapons, both missiles and aircraft. Thor, based in the UK, would likely have more warning of an impending attack.{{efn|The Army noted that an overwater approach to the UK meant that Thor had little warning at all.}} This is precisely the reason that the Army spent considerable effort on making Jupiter mobile, in order to make surprise attacks difficult without prior [[aerial reconnaissance]] missions.{{sfn|Mackenzie|1993|p=131}}

However, in November 1958, the Air Force decided Jupiter would be launched from fixed emplacements. Army General [[Maxwell Taylor]] argued this was done deliberately, noting that:

{{cquote|...a mobile missile needs Army-type troops to move, emplace, protect and fire it... a decision to organize mobile ballistic missile units would in logic have led to transferring the operational use of the weapon back to the Army – where it should have been all the time.{{sfn|Mackenzie|1993|p=131}}}}

To offset the possibility of air attack, the systems were upgraded to allow a launch within 15 minutes of a launch order.{{sfn|Kyle|2011|loc= Air Force Gains Control}}

==Testing history==
Rocketdyne tested the first S-3 engine at their Santa Susana, California facilities in November 1955. A mock-up was delivered to ABMA in January 1956, followed by the first prototype engines in July 1956. Testing of these engines began in September 1956 at ABMA's new Power Plant Test Stand. This demonstrated a number of problems with unstable combustion, leading to the failure of four engines by November. To continue testing, the engine was temporarily derated back to 135,000&nbsp;lbf and was successfully tested at this level in January 1957. Continued work on the engine developed several sub-versions, finally reaching the design goal of 150,000&nbsp;lbf in the S-3D model.{{sfn|Kyle|2011|loc=Testing Jupiter, Propulsion}}

The 135,000 pound engine, also used in the first Thor and Atlas tests, had conical thrust chambers, but the 150,000 pound model switched to bell-shaped thrust chambers. Unlike Thor and Atlas, which had two small vernier engines for roll control, Jupiter gimbaled the turbine exhaust. The early test model Jupiters had two small gas jets powered off the turbine exhaust, the gimbaled exhaust pipe not being introduced until late 1958.{{citation_needed|date=July 2019}}

===Static tests===
In 1954 Test Laboratory director [[Karl Heimburg]] began construction of the Static Test Stand for Redstone testing. This was still under construction when it was re-purposed for Jupiter, and finally completed in January 1957.{{sfn|Kyle|2011|loc=Testing Jupiter, Static Test}} A Jupiter was installed in the stand that month, and fired for the first time on 12 February 1957. This almost ended in disaster when a small explosion went off in the [[liquid oxygen]] (LOX) pump, and as the missile sat there the LOX boiled off and threatened to burst the tanks. The day was saved when the foreman, Paul Kennedy, ran to the missile and connected a pressure line to drain the oxygen buildup in the tank. The problem was later traced to the lubricant used in the pump, which tended to burst into flames in contact with LOX. A new lubricant was introduced, along with a series of changes to the test stand to help retain control in these situations.<ref>{{cite web |first=Harry |last=Johnstone |title=The Life and Times of Harry M. Johnstone |url=http://www.enginehistory.org/hjohnstone.shtml |website=Engine History |url-status=dead |archive-url=https://web.archive.org/web/20150924001008/http://www.enginehistory.org/hjohnstone.shtml |archive-date=24 September 2015 |df=dmy-all }}</ref>

===Flight tests===
Kurt Debus had led the construction of launch pads for Redstone missiles at [[Cape Canaveral, Florida]], building the twin LC-5 and LC-6 pads about {{convert|500|feet}} apart with a common [[blockhouse]] located {{convert|300|feet}} away between the two. Redstone testing moved to these pads from the smaller LC-4 on 20 April 1955, with the launch of the seventh Redstone from LC-6. Envisioning an extended test program, a second set of similar pads began construction in 1956, LC-26 A and B; the only major difference was the blockhouse was located slightly further away, about {{convert|400|feet}}. In late 1957 a set of parallel railway tracks running just east of the pads was added, allowing an A-frame gantry to be rolled to any of the four pads.{{sfn|Kyle|2011|loc=The Cape}}

Jupiters were delivered to the Cape strapped to wheeled trailers and flown to the Cape's "Skid Strip" on C-124s. They were then moved to Hangar R at the Cape Industrial Area where the nose cone was mated with the missile, and electrical checkout was performed. It was then moved on the trailer to the pads, about {{convert|3.5|miles}} south, where they were lifted to vertical by a crane on the movable gantry. Just to the north of the launch area was the Air Force's LC-17 for Thor, and LC-18 used for Thor and the Navy's [[Vanguard (rocket)|Vanguard]]. After the Army's head start, the Air Force had since caught up and attempted its first Thor launch on 26 January 1957, which ended with the missile exploding on the launch pad.{{sfn|Kyle|2011|loc=Jupiter Takes Flight}}

Jupiter test flights commenced with the launch of AM-1A (ABMA Missile 1A) on 1 March 1957 from LC-5. This missile was equipped with the lower-thrust interim engine. The vehicle performed well until past 50 seconds into launch when control started to fail, leading to breakup at T+73 seconds. It was deduced that turbopump exhaust was sucked up by the partial vacuum in the area behind the missile and began to burn in the tail section. The heat burned through the control wiring, so extra insulation was added there on future flights. An identical AM-1B was quickly readied and launched on 26 April. AM-1B's flight went entirely according to plan up to T+70 seconds when the missile started becoming unstable in flight and finally broke up at T+93 seconds. The failure was deduced to have been the result of propellant slosh due to bending modes induced by the steering maneuvers needed to perform the flight trajectory. The solution to this problem involved testing several types of [[slosh baffle]]s in a Jupiter center section until discovering a suitable type for both the LOX and fuel tanks.{{sfn|Kyle|2011|loc=Jupiter Takes Flight}}

The third Jupiter, also numbered AM-1, was quickly equipped with the baffles and launched on 31 May, slightly over a month after AM-1B, traveling a full {{convert|1247|nmi}} downrange. This version had a slightly improved S-3 engine with {{convert|139000|lbf}} thrust. AM-2 flew from LC-26A on 28 August, and successfully tested the separation of the rocket body from the reentry vehicle section before splashing down at {{convert|1460|nmi}}. AM-3 flew from LC-26B on 23 October, including the ablative heat shield and the new ST-90 INS. This test flew a planned distance of {{convert|1100|nmi}}.{{sfn|Kyle|2011|loc=Jupiter Takes Flight}}

AM-3A launched on 26 November and all went according to plan until T+101 seconds when engine thrust abruptly terminated. The missile broke up at T+232 seconds. On 18 December, AM-4 lost thrust T+117 seconds and fell into the ocean {{convert|149|nmi}} downrange. These failures were traced to an inadequate turbopump design that resulted in a string of failures in the Jupiter, Thor, and Atlas programs, all of which used a variant of the same Rocketdyne engine. Testing then paused for five months while Rocketdyne came up with a number of fixes and the Army retrofitted all its Jupiters with the redesigned pumps.{{sfn|Kyle|2011|loc=Jupiter Takes Flight}} In spite of these failures, Jupiter was declared operational on 15 January 1958.

Taking the time to also fully rate the engine to 150,000&nbsp;lbf, the new engine was first flown on AM-5 on 18 May 1958 from LC-26B, reaching a planned {{convert|1247|nmi}}. AM-5 also carried the real nose cone design, which separated from the rocket body, spun up the warhead, and separated to allow the warhead to continue on its own. The warhead section was equipped with a parachute and was recovered by the Navy some {{convert|28|nmi}} from its predicted splashdown point.{{sfn|Kyle|2011|loc=Jupiter Takes Flight}}

AM-6B included both the production nose cone and the ST-90 INS during its launch from LC-26B on 17 July 1958. This time the Navy recovered it only {{convert|1.5|nmi}} from its planned splashdown point {{convert|1241|nmi}} downrange. AM-7 flew {{convert|1207|nmi}} on 27 August, testing a new solid fuel rocket for spinup, replacing the older hydrogen peroxide model. AM-9 was launched on 10 October, the first Jupiter to carry the fully functional turbine exhaust roll control system. The flight failed however; a pinhole leak in the thrust transducer area started a thrust section fire and loss of vehicle control. The missile tumbled and broke up at T+49 seconds.{{Sfn|Kyle|2011|loc=Jupiter Takes Flight}}

Afterwards, there was only one more failure in the Jupiter program, AM-23 on 15 September 1959, which developed a leak in a nitrogen bottle that led to depressurization of the RP-1 tank and almost immediate loss of control at liftoff. The missile wobbled from side to side and the RP-1 tank began to break apart starting at T+7 seconds. The Jupiter flipped upside down, dumping out the contents of the RP-1 tank, followed by total vehicle breakup at T+13 seconds, just before the Range Safety Officer could issue the flight termination command. Flying debris struck and damaged a Juno II on the adjacent LC-5. This particular launch was carrying a biological nose cone with mice and other specimens (which did not survive).<ref>{{cite web |url=http://www.astronautix.com/lvs/jupiter.htm |title=Jupiter |website=Encyclopedia Astronautica |first=Andreas |last=Parsch |access-date=26 April 2014 |url-status=dead |archive-url=https://web.archive.org/web/20111010114842/http://astronautix.com/lvs/jupiter.htm |archive-date=10 October 2011 |df=dmy-all }}</ref>

Through the early 1960s, a number of Jupiters were launched by the forces of other countries, as well as the Air Force, as part of ongoing combat training. The last launch of this sort was by the Italian Air Force, CM-106, which took place from LC-26B on 23 January 1963.<ref>{{cite web |first=Mark |last=Wade |url=http://www.astronautix.com/fam/jupiter.htm |title=Jupiter |website=Encyclopedia Astronautica |url-status=dead |archive-url=https://web.archive.org/web/20170404043240/http://www.astronautix.com/fam/jupiter.htm |archive-date=4 April 2017 |df=dmy-all }}</ref>

===Biological flights===
[[File:Jupiter AM-18 pre-launch.jpg|thumb|195x195px|Jupiter AM-18 pre-launch]]
[[File:Able baker 01.jpg|thumb|191x191px|Able and [[Miss Baker|Baker]], the first two primates who survived space travel aboard Jupiter AM-18.]]

Jupiter missiles were used in a series of [[Monkeys in space|suborbital biological test flights]]. On 13 December 1958, Jupiter AM-13 was launched from [[Cape Canaveral Air Force Station|Cape Canaveral]], Florida with a Navy-trained South American [[squirrel monkey]] named [[Gordo (monkey)|Gordo]] on board. The nose cone recovery parachute failed to operate and Gordo did not survive the flight. Telemetry data sent back during the flight showed that the monkey survived the {{cvt|10|g-force|round=10}} of launch, eight minutes of weightlessness and {{cvt|40|g-force|round=10}} of reentry at {{cvt|10,000|mph|km/s|1}}. The nose cone sank {{convert|1302|nmi|km|abbr=out}} downrange from Cape Canaveral and was not recovered.

Another biological flight was launched on 28 May 1959. Aboard Jupiter AM-18 were a {{cvt|7|lb|kg|1}} American-born [[rhesus monkey]], Able, and an {{cvt|11|oz|g|round=10}} South American [[squirrel monkey]], [[Miss Baker|Baker]]. The monkeys rode in the nose cone of the missile to an altitude of {{convert|300|mi|km|abbr=}} and a distance of {{convert|1500|mi|km}} down the [[Atlantic Missile Range]] from Cape Canaveral.<ref>{{Cite report|last1=Beischer, DE|last2=Fregly, AR|date=1962|title=Animals and man in space. A chronology and annotated bibliography through the year 1960.|url=http://archive.rubicon-foundation.org/9288|language=en|access-date=30 June 2019|archive-date=11 August 2015|archive-url=https://web.archive.org/web/20150811085105/http://archive.rubicon-foundation.org/xmlui/handle/123456789/9288|url-status=usurped}}</ref> They withstood accelerations of {{cvt|38|g-force|round=10}} and were weightless for about nine minutes. A top speed of {{cvt|10,000|mph|km/s|1}} was reached during their 16-minute flight.

After [[splashdown (spacecraft landing)|splashdown]] the Jupiter nosecone carrying Able and Baker was recovered by the seagoing tug [[USS Kiowa (AT-72)|USS ''Kiowa'']] (ATF-72). The monkeys survived the flight in good condition. Able died four days after the flight from a reaction to anesthesia while undergoing surgery to remove an infected medical electrode. Baker lived for many years after the flight, finally succumbing to kidney failure on 29 November 1984 at the [[United States Space and Rocket Center]] in [[Huntsville, Alabama|Huntsville]], Alabama.

=== Mercury-Jupiter ===
[[File:Jupiter atlas redstone rockets comparison.jpg|alt=Mercury-Jupiter (center) compared with Redstone (left) and Atlas (right).|thumb|Mercury-Jupiter (center) compared with Redstone (left) and Atlas (right). Mercury-Jupiter was a proposal, and not launched.]]

'''Mercury-Jupiter''' was a proposed suborbital launch configuration consisting of a Jupiter missile carrying a Mercury capsule. Two flights were planned in support of [[Project Mercury]]. On July 1, 1959, less than a year after the October, 1958 program start date, the flights were canceled due to budget constraints.<ref>{{cite web |url=https://history.nasa.gov/SP-4001/p2a.htm |title=Project Mercury – A Chronology – PART II (A) Research and Development Phase of Project Mercury |first=James M. |last=Grimwood |website=NASA |id=NASA SP-4001 |access-date=2024-03-01}}</ref> The MJ-1 flight would have been a heat shield test. The MJ-2 flight was planned as a maximum dynamic pressure qualification test of the production Mercury spacecraft with a chimpanzee on board.<ref>{{cite web |url=http://astronautix.com/flights/merr2mj2.htm |website=Encyclopedia Astronautica |title=Mercury-Jupiter MJ-2 |archive-url=https://web.archive.org/web/20111013154511/http://astronautix.com/flights/merr2mj2.htm |archive-date=2011-10-13}}</ref>

==Operational deployment==
[[File:864th Strategic Missile Squadron.PNG|right|thumb|125px|864th SMS insignia]]

In April 1958, under the command of [[Dwight D. Eisenhower|President Eisenhower]], the U.S. [[United States Department of Defense|Department of Defense]] notified the Air Force it had tentatively planned to deploy the first three Jupiter squadrons (45 missiles) in France. However, in June 1958 the new French President [[Charles de Gaulle]] refused to accept basing any Jupiter missiles in France. This prompted U.S. to explore the possibility of deploying the missiles in Italy and Turkey. The Air Force was already implementing plans to base four squadrons (60 missiles) under [[Project Emily]] —subsequently redefined as 20 [[Royal Air Force]] squadrons each with three missiles—of [[PGM-17 Thor]] IRBMs in Britain on airfields stretching from [[Yorkshire]] to [[East Anglia]].

In 1958, the United States Air Force activated the [[864th Strategic Missile Squadron]] at ABMA. Although the USAF briefly considered training its Jupiter crews at [[Vandenberg AFB]], California, it later decided to conduct all of its training at [[Huntsville, Alabama|Huntsville]]. In June and September of the same year the Air Force activated two more squadrons, the 865th and 866th.

In April 1959, the secretary of the Air Force issued implementing instructions to USAF to deploy two Jupiter squadrons to Italy. The two squadrons, totaling 30 missiles, were deployed at 10 sites in Italy from 1961 to 1963. They were operated by [[Aeronautica Militare Italiana|Italian Air Force]] crews, but USAF personnel controlled arming the nuclear warheads. The deployed missiles were under command of [[36th Air Brigade (Italy)|36th Strategic Interdiction Air Brigade]] (''36ª Aerobrigata Interdizione Strategica'', Italian Air Force) at [[Gioia del Colle Air Base]], Italy.

In October 1959, the location of the third and final Jupiter MRBM squadron was settled when a government-to-government agreement was signed with Turkey. The U.S. and Turkey concluded an agreement to deploy one Jupiter squadron on NATO's southern flank. One squadron totaling 15 missiles was deployed at five sites near [[İzmir]], Turkey from 1961 to 1963, operated by USAF personnel, with the first flight of three Jupiter missiles turned over to the Türk Hava Kuvvetleri (Turkish Air Force) in late October 1962, but USAF personnel retaining control of nuclear warhead arming.

On four occasions between mid-October 1961 and August 1962, Jupiter mobile missiles carrying 1.4 megatons of TNT (5.9 PJ) nuclear warheads were struck by lightning at their bases in Italy. In each case, thermal batteries were activated, and on two occasions, [[tritium]]-[[deuterium]] [[Boosted fission weapon|"boost" gas]] was injected into the warhead [[Pit&nbsp;(nuclear weapon)|pit]]s, partially arming them. After the fourth lightning strike on a Jupiter MRBM, the USAF placed protective lightning strike-diversion tower arrays at all of the Italian and Turkish Jupiter MRBM missiles sites.

In 1962, a Bulgarian [[MiG-17]] reconnaissance airplane was reported to have crashed into an olive grove near one of the U.S. Jupiter missile launch sites in Italy, after overflying the site.<ref>{{cite web|last=Lednicer |first=David|title=Intrusions, Overflights, Shootdowns and Defections During the Cold War and Thereafter|url=http://mysite.ncnetwork.net/res12e522/ColdWar.html|website=Aviation History Pages|access-date=16 January 2011|date=9 December 2010}}</ref>

By the time the Turkish Jupiters had been installed, the missiles were already largely obsolete and increasingly vulnerable to Soviet attacks.<ref>{{Cite book |last=Plokhy |first=Serhii |title=Nuclear Folly. A New History of the Cuban Missile Crisis |publisher=Penguin Books |year=2022 |pages=214, 217}}</ref> All Jupiter MRBMs were removed from service by April 1963, as a backdoor trade with the Soviets in exchange for their [[Cuban Missile Crisis|earlier removal of MRBMs from Cuba]].

===Deployment sites===
{{geoGroup}}
;United States
[[Redstone Arsenal]], Huntsville, Alabama:
*{{Coord|34|37|58.11|N|86|39|56.40|W|display=inline}}

[[White Sands Missile Range]], New Mexico:
*{{Coord|32|52|47.45|N|106|20|43.64|W|display=inline}}

;Republic of Italy
[[File:Jupiter Deployment Italy.jpg|right|thumb|Deployment locations for Jupiter missiles in Italy from 1961 to 1963]]

Headquarters: [[Gioia del Colle Air Base]], the launch sites (built in a triangular configuration) were in the direct vicinity of the villages [[Acquaviva delle Fonti]], [[Altamura]] (two sites), [[Gioia del Colle]], [[Gravina in Puglia]], [[Laterza, Apulia|Laterza]], [[Mottola]], [[Spinazzola]], [[Irsina]] and [[Matera]]:
*Training Pad {{Coord|40|47|6.74|N|16|55|33.5|E|display=inline}}

Squadron 1:
*Site 1 {{Coord|40|44|24.59|N|16|55|58.83|E|display=inline}}
*Site 3 {{Coord|40|35|42.00|N|16|51|33.00|E|display=inline}}
*Site 4 {{Coord|40|48|47.05|N|16|22|53.08|E|display=inline}}
*Site 5 {{Coord|40|45|32.75|N|16|22|53.08|E|display=inline}}
*Site 7 {{Coord|40|57|43.98|N|16|10|54.66|E|display=inline}}

Squadron 2:
*Site 2 {{Coord|40|40|42.00|N|17|6|12.03|E|display=inline}}
*Site 6 {{Coord|40|58|6.10|N|16|30|22.73|E|display=inline}}
*Site 8 {{Coord|40|42|14.98|N|16|8|28.42|E|display=inline}}
*Site 9 {{Coord|40|55|23.40|N|16|48|28.54|E|display=inline}}
*Site 10 {{Coord|40|34|59.77|N|16|35|43.26|E|display=inline}}

;Turkish Republic
Headquarters: [[Izmir Air Base|Çiğli Air Base]]:
*Training Pad {{Coord|38|31|17.32|N|27|1|3.89|E|display=inline}}
*Site 1 {{Coord|38|42|26.68|N|26|53|4.13|E|display=inline}}
*Site 2 {{Coord|38|42|23.76|N|27|53|57.66|E|display=inline}}
*Site 3 {{Coord|38|50|37.66|N|27|02|55.58|E|display=inline}}
*Site 4 {{Coord|38|44|15.13|N|27|24|51.46|E|display=inline}}
*Site 5 {{Coord|38|47|30.73|N|27|42|28.94|E|display=inline}}

==Description==
[[File:Jupiter IRBM.jpg|thumb|right|Jupiter with its "petal" cover open.]]
[[File:Jupiter reentery vehicle.jpg|thumb|Jupiter was designed in an era when nuclear weapons were still very large and heavy. Its large reentry vehicle is typical of missile designs of the 1950s.]]

Jupiter squadrons consisted of 15 missiles and approximately 500 military personnel with five "flights" of three missiles each, manned by five officers and 10 NCOs. To reduce vulnerability, the flights were located approximately 30 miles apart, with the triple launcher emplacements separated by a distance of several hundred miles.

The ground equipment for each emplacement was housed in approximately 20 vehicles; including two generator trucks, a power distribution truck, short- and long-range [[theodolite]]s, a hydraulic and pneumatic truck and a liquid oxygen truck. Another trailer carried 6000 gallons of fuel and three liquid oxygen trailers each carried {{convert|4000|gal}}.

The missiles arrived at the emplacement on large trailers; while still on the trailer, the crew attached the hinged launch pedestal to the base of the missile which was hauled to an upright position using a winch. Once the missile was vertical, fuel and oxidizer lines were connected and the bottom third of the missile was encased in a "flower petal shelter", consisting of wedge-shaped metal panels, allowing crew members to service the missiles in all weather conditions. Stored empty, on 15-minute combat status in an upright position on the launch pad, the firing sequence included filling the fuel and oxidizer tanks with {{convert|68000|lbs|kg|abbr=on|sigfig=2}} of LOX and {{convert|30000|lbs|kg|abbr=on|sigfig=2}} of RP-1, while the guidance system was aligned and targeting information loaded. Once the fuel and oxidizer tanks were full, the launch controlling officer and two crewmen in a mobile launch control trailer could launch the missiles.

Each squadron was supported by a receipt, inspection and maintenance (RIM) area to the rear of the emplacements. RIM teams inspected new missiles and provided maintenance and repair to missiles in the field. Each RIM area also housed 25 tons of liquid oxygen and nitrogen generating plants. Several times a week, tanker trucks carried the fuel from the plant to the individual emplacements.

==Specifications (Jupiter MRBM)==
* Length: 60&nbsp;ft (18.3 m)
* Diameter: 8&nbsp;ft 9 in (2.67 m)
* Total Fueled Weight: 108,804&nbsp;lb (49,353&nbsp;kg)
* Empty Weight: 13,715&nbsp;lb (6,221&nbsp;kg)
* Oxygen (LOX) Weight: 68,760&nbsp;lb (31,189&nbsp;kg)
* RP-1 (kerosene) Weight: 30,415&nbsp;lb (13,796&nbsp;kg)
* Thrust: 150,000&nbsp;lbf (667&nbsp;kN)
* Engine: [[Rocketdyne S-3D|Rocketdyne LR79-NA]] (Model S-3D)
* ISP: 247.5 s (2.43&nbsp;kN·s/kg)
* Burning time: 2 min. 37 sec.
* Propellant consumption rate: 627.7&nbsp;lb/s (284.7&nbsp;kg/s)
* Range: {{convert|1,500|mi|km|abbr=on}}
* Flight time: 16 min 56.9 sec
* Cutoff velocity: 8,984&nbsp;mph (14,458&nbsp;km/h) – Mach 13.04
* Reentry velocity: 10,645&nbsp;mph (17,131&nbsp;km/h) – Mach 15.45
* Acceleration: 13.69 ''g'' (134&nbsp;m/s<sup>2</sup>)
* Peak deceleration: 44.0 ''g'' (431&nbsp;m/s<sup>2</sup>)
* Peak altitude: {{convert|390|mi|km|abbr=on}}
* CEP 4,925&nbsp;ft (1,500 m)
* Warhead: 1.45 Mt Thermonuclear [[W49]] – 1,650&nbsp;lb (750&nbsp;kg)
* Fusing: Proximity and Impact
* Guidance: Inertial

==Launch vehicle derivatives==
[[File:Jupiter-C vs Jupiter IRBM.jpg|right|thumb|Illustration showing differences among Redstone, Jupiter-C, Mercury-Redstone, and Jupiter IRBM.]]

The [[Saturn I]] and [[Saturn IB]] rockets first stage was manufactured using the tooling from Jupiter and Redstone production, consisting of a central tank of the same diameter of the Jupiter missile with eight tanks of the same diameter as the Redstone clustered around it, all containing LOX/RP-1.

The Jupiter MRBM was also modified by adding upper stages, in the form of clustered [[MGM-29 Sergeant|Sergeant]]-derived rockets, to create a space launch vehicle called [[Juno II]], not to be confused with the [[Juno I]] which was a Redstone-Jupiter-C missile development. There is also some confusion with another U.S. Army rocket called the [[Jupiter-C]], which were Redstone missiles modified by lengthening the fuel tanks and adding small solid-fueled upper stages.

===Specifications (Juno II launch vehicle)===
{{Main|Juno II}}
[[File:Juno II rocket.jpg|right|thumb|Juno II launch vehicle derived from Jupiter IRBM mobile missile.]]

The Juno II was a four-stage rocket derived from the Jupiter IRBM. It was used for 10 satellite launches, six of which failed. It launched [[Pioneer 3]] (a partial success), [[Pioneer 4]], [[Explorer 7]], [[Explorer 8]], and [[Explorer 11]].
* Juno II total length: 24.0 m
* Orbit payload to 200&nbsp;km: 41&nbsp;kg
* Escape velocity payload: 6&nbsp;kg
* First launch date: 6 December 1958
* Last launch date: 24 May 1961

{| class="wikitable"
! Parameter
! First stage
! Second stage
! Third stage
! Fourth stage
|-
| Gross mass
| 54,431&nbsp;kg
| 462&nbsp;kg
| 126&nbsp;kg
|  42&nbsp;kg
|-
| Empty mass
| 5,443&nbsp;kg
|   231&nbsp;kg
|    63&nbsp;kg
|    21&nbsp;kg
|-
| Thrust
| 667&nbsp;kN
|  73&nbsp;kN
|  20&nbsp;kN
|   7&nbsp;kN
|-
| Isp
| 248 s<br />(2.43&nbsp;kN·s/kg)
| 214 s<br />(2.10&nbsp;kN·s/kg)
| 214 s<br />(2.10&nbsp;kN·s/kg)
| 214 s<br />(2.10&nbsp;kN·s/kg)
|-
| Burn time
| 182 s
| 6 s
| 6 s
| 6 s
|-
| Length
| 18.28 m
| 1.0 m
| 1.0 m
| 1.0 m
|-
| Diameter
| 2.67 m
| 1.0 m
| 0.50 m
| 0.30 m
|-
| Engine:
| Rocketdyne S-3D
| Eleven Sergeants
| Three Sergeants
| One Sergeant
|-
| Propellant
| LOX/RP-1
| Solid Fuel
| Solid Fuel
| Solid fuel
|}

==Jupiter MRBM and Juno II launches==
There were 46 test launches, all launched from [[Cape Canaveral Air Force Station|Cape Canaveral Missile Annex]], Florida.<ref>{{cite web|last=Wade|first=Mark|title=Juno II|url=http://www.astronautix.com/lvs/junoii.htm|website=Encyclopedia Astronautica|access-date=16 January 2011|url-status=dead|archive-url=https://web.archive.org/web/20101129085534/http://astronautix.com/lvs/junoii.htm|archive-date=29 November 2010|df=dmy-all}}</ref>

===1957===
{| class="wikitable" style="margin: 1em 1em 1em 0"
|-
! Date/Time<br/>([[UTC]])
! Rocket
! [[Serial number|S/N]]
! Launch Site
! Payload
! Function
! Orbit
! Outcome
! Remarks
|-
|1957-03-01
|Jupiter
|AM-1A
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|
|Missile test
|Suborbital
|{{Failure}}
|First flight of Jupiter. Thrust section overheating led to control failure and missile breakup T+74 seconds.
|-
|1957-04-26
|Jupiter
|AM-1B
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|
|Missile test
|Suborbital
|{{Failure}}
|Propellant slosh led to control failure and missile breakup T+93 seconds.
|-
|1957-05-31
|Jupiter
|AM-1
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1957-08-28
|Jupiter
|AM-2
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1957-10-23
|Jupiter
|AM-3
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1957-11-27
|Jupiter
|AM-3A
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Failure}}
|Turbopump failure caused loss of thrust T+101 seconds. Missile broke up T+232 seconds.
|-
|1957-12-19
|Jupiter
|AM-4
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Failure}}
|Turbopump failure caused loss of thrust T+116 seconds. Missile remained structurally intact until impact with the ocean.
|-
|}

===1958===
{| class="wikitable" style="margin: 1em 1em 1em 0"
|-
! Date/Time<br/>([[UTC]])
! Rocket
! [[Serial number|S/N]]
! Launch Site
! Payload
! Function
! Orbit
! Outcome
! Remarks
|-
|1958-05-18
|Jupiter
|AM-5
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1958-07-17
|Jupiter
|AM-6B
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1958-08-27
|Jupiter
|AM-7
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1958-10-10
|Jupiter
|AM-9
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Failure}}
|Hot exhaust gas leak caused thrust section fire and loss of control followed by vehicle breakup T+49 seconds.
|-
|1958-12-06
|Juno II
|AM-11
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|[[Pioneer 3]]
|Lunar orbiter
|''High suborbital''
|{{Partial failure}}
|Premature first stage cutoff
|-
|1958-12-13
|Jupiter
|AM-13
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Biological nose cone w/ squirrel monkey
|Missile test
|Suborbital
|{{Partial failure}}
|Parachute failed on payload, resulting in death of squirrel monkey occupant. Telemetry was received during the flight, and the squirrel monkey did survive launch and re-entry.
|-
|}

===1959===
{| class="wikitable" style="margin: 1em 1em 1em 0"
|-
! Date/Time<br/>([[UTC]])
! Rocket
! [[Serial number|S/N]]
! Launch Site
! Payload
! Function
! Orbit
! Outcome
! Remarks
|-
|1959-01-22
|Jupiter
|CM-21
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|
|Missile test
|Suborbital
|{{Success}}
|First flight of production Chrysler-built Jupiter
|-
|1959-02-27
|Jupiter
|CM-22
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-03-03
|Juno II
|AM-14
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|[[Pioneer 4]]
|Lunar orbiter
|TEO
|{{Success}}
|First successful American lunar probe
|-
|1959-04-04
|Jupiter
|CM-22A
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-05-07
|Jupiter
|AM-12
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-05-14
|Jupiter
|AM-17
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-05-28
|Jupiter
|AM-18
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Biological nose cone
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-07-16
|Juno II
|AM-16
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|Explorer 6
|Scientific
|LEO
|{{Failure}}
|Electrical short in the guidance system caused loss of control at liftoff. RSO T+5 seconds.
|-
|1959-08-14
|Juno II
|AM-19B
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Beacon 2
|Scientific
|LEO
|{{Failure}}
|Premature first stage cutoff
|-
|1959-08-27
|Jupiter
|AM-19
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-09-15
|Jupiter
|AM-23
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Biological nose cone
|Missile test
|Suborbital
|{{Failure}}
|Pressure gas leak led to loss of control at liftoff. Missile self-destructed T+13 seconds.
|-
|1959-10-01
|Jupiter
|AM-24
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 6|LC-6]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-10-13
|Juno II
|AM-19A
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 5|LC-5]]
|Explorer 7
|Scientific
|LEO
|{{Success}}
|
|-
|1959-10-22
|Jupiter
|AM-31
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-11-05
|Jupiter
|CM-33
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 6|LC-6]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-11-19
|Jupiter
|AM-25
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-12-10
|Jupiter
|AM-32
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 6|LC-6]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1959-12-17
|Jupiter
|AM-26
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|}

===1960===
{| class="wikitable" style="margin: 1em 1em 1em 0"
|-
! Date/Time<br/>([[UTC]])
! Rocket
! [[Serial number|S/N]]
! Launch Site
! Payload
! Function
! Orbit
! Outcome
! Remarks
|-
|1960-01-26
|Jupiter
|AM-28
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1960-03-23
|Juno II
|AM-19C
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Explorer
|Scientific
|LEO
|{{Failure}}
|Third stage failed to ignite
|-
|1960-10-20
|Jupiter
|CM-217
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1960-11-03
|Juno II
|AM-19D
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Explorer 8
|Scientific
|LEO
|{{Success}}
|
|-
|}

===1961===
{| class="wikitable" style="margin: 1em 1em 1em 0"
|-
! Date/Time<br/>([[UTC]])
! Rocket
! [[Serial number|S/N]]
! Launch Site
! Payload
! Function
! Orbit
! Outcome
! Remarks
|-
|1961-02-25
|Juno II
|AM-19F
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Explorer 10
|Scientific
|LEO
|{{Failure}}
|Third stage failed to ignite
|-
|1961-04-22
|Jupiter
|CM-209
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1961-04-27
|Juno II
|AM-19E
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Explorer 11
|Scientific
|LEO
|{{Success}}
|
|-
|1961-05-24
|Juno II
|AM-19G
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26B]]
|Explorer 12
|Scientific
|LEO
|{{Failure}}
|Second stage failed to ignite. Final flight of Juno II
|-
|1961-08-05
|Jupiter
|CM-218
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1961-12-06
|Jupiter
|CM-115
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|}

===1962===
{| class="wikitable" style="margin: 1em 1em 1em 0"
|-
! Date/Time<br/>([[UTC]])
! Rocket
! [[Serial number|S/N]]
! Launch Site
! Payload
! Function
! Orbit
! Outcome
! Remarks
|-
|1962-04-18
|Jupiter
|CM-114
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|1962-08-01
|Jupiter
|CM-111
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|
|-
|}

===1963===
{| class="wikitable" style="margin: 1em 1em 1em 0"
|-
! Date/Time<br/>([[UTC]])
! Rocket
! [[Serial number|S/N]]
! Launch Site
! Payload
! Function
! Orbit
! Outcome
! Remarks
|-
|1963-01-22
|Jupiter
|CM-106
|[[Cape Canaveral Air Force Station|CCAFS]] [[Cape Canaveral Air Force Station Launch Complex 26|LC-26A]]
|
|Missile test
|Suborbital
|{{Success}}
|Final flight of Jupiter
|-
|}

==Former operators==
[[File:PGM-19 operators.png|thumb|400px|Map with former PGM-19 operators in red]]

;{{USA}}: [[United States Air Force]]
* [[864th Strategic Missile Squadron]]
* [[865th Strategic Missile Squadron]]
* [[866th Strategic Missile Squadron]]

;{{Flagicon|Italy}} Italy:''[[Aeronautica Militare]]'' ([[Italian Air Force]])
* ''[[36ª Brigata Aerea Interdizione Strategica]]'' (36th Strategic Air Interdiction Brigade)

;{{Flagicon|Turkey}} Turkey:''[[Türk Hava Kuvvetleri]]'' ([[Turkish Air Force]])

==Surviving examples==
Some Jupiter and Juno II are on display:

* [[File:MSFC rocket park.jpg|PGM-19 Jupiter directly in front of a Saturn I, [[Marshall Space Flight Center]]|thumb]]The [[Marshall Space Flight Center]] in [[Huntsville, Alabama]] displays a Jupiter missile in its Rocket Garden.
* [[File:USSRC Rocket Park.JPG|Jupiter IRBM and Juno II (second and thirds from left) at the [[USSRC|United States Space & Rocket Center]]|thumb]]The [[U.S. Space & Rocket Center]] in [[Huntsville, Alabama]] displays two Jupiters, including one in [[Juno II]] configuration, in its Rocket Park.
* [[File:Juno II - Kennedy Space Center - Cape Canaveral, Florida - DSC02531.jpg|Juno II at Kennedy Space Center |thumb]]A Jupiter (in [[Juno II]] configuration) is displayed in the Rocket Garden at [[Kennedy Space Center]], Florida.  It was damaged by [[Hurricane Frances]] in 2004,<ref>{{cite web |title=Hurricane Frances damage to Kennedy Space Center |url=http://www.collectspace.com/ubb/Forum41/HTML/000220.html |access-date=24 February 2012 |website=collect SPACE}}</ref> but was repaired and subsequently placed back on display.
* [[File:Chrysler SM-78 - PGM-19A USAF.jpg|PGM-19 Jupiter at the [[National Museum of the United States Air Force]]|thumb]]A PGM-19 is on display at the [[National Museum of the United States Air Force]] in [[Dayton, Ohio]].<ref>{{cite web |title=Factsheets : Chrysler SM-78/PGM-19A Jupiter |url=http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=534 |url-status=dead |archive-url=https://web.archive.org/web/20140407094736/http://www.nationalmuseum.af.mil/factsheets/factsheet.asp?id=534 |archive-date=7 April 2014 |access-date=26 April 2014 |publisher=National Museum of the United States Air Force |df=dmy-all}}</ref>
* [[File:F-89J Hampton Air Power Park VA 2007.jpg|SM-78 Jupiter at [[Air Power Park]]|thumb]][[Air Power Park]] in [[Hampton, Virginia]] displays an SM-78.
* An SM-78/PMG-19 is on display at the [[Air Force Space & Missile Museum]] at [[Cape Canaveral, Florida]]. The missile had been present in the rocket garden for many years until 2009 when it was taken down and given a complete restoration.<ref>{{cite web |url=http://www.afspacemuseum.org/displays/Jupiter/index.htm |title=Jupiter |publisher=Air Force Space and Missile Museum |location=Cape Canaveral, Florida |access-date=26 April 2014 |archive-date=19 April 2014 |archive-url=https://web.archive.org/web/20140419025550/http://www.afspacemuseum.org/displays/Jupiter/index.htm |url-status=dead }}</ref> This pristine artifact is now in sequestered storage in Hangar R on Cape Canaveral AFS and cannot be viewed by the general public.
* A PGM-19 is on display at the South Carolina State Fairgrounds in [[Columbia, South Carolina]]. The missile, named ''Columbia'', was presented to the city in the early 1960s by the US Air Force. It was installed at the fairgrounds in 1969 at a cost of $10,000.<ref>{{cite news |url=http://www.thestate.com/2010/10/06/1499016/the-2010-sc-state-fair-is-just.html |title=The 2010 SC State Fair is just a week away |archive-url=https://web.archive.org/web/20101007231001/http://www.thestate.com/2010/10/06/1499016/the-2010-sc-state-fair-is-just.html |archive-date=7 October 2010 |url-status=dead |last=Rantin |first=Bertram |work=The State |location=South Carolina |date=6 October 2010 |access-date=26 April 2014}}</ref>
* The [[Virginia Museum of Transportation]] in downtown [[Roanoke, Virginia]] displays a Jupiter PGM-19.
* The [[Frontiers of Flight Museum]] at [[Dallas Love Field]] in Dallas, Texas, has a Jupiter missile on display outdoors.




==See also==
* [[List of United States Air Force missile squadrons]]
* [[List of missiles]]
* [[M-numbers]]
* [[Strategic Air Command]]
* [[Theatre ballistic missile]]s

==Notes==
{{notelist}}

==References==
===Citations===
{{Reflist}}

===Bibliography===
*{{cite web |first=Roger |last=Bilstein |url=https://history.nasa.gov/SP-4206/ch2.htm |title=Stages to Saturn  |date=1996 |publisher=NASA History Office }}
*{{cite tech report |first=Roy |last=Healy |title=Development of the Rocket Engine for the Jupiter Missile |url=http://heroicrelics.org/info/jupiter/devel-of-jupiter-engine/Development%20of%20the%20Rocket%20Engine%20for%20the%20Jupiter%20Missile%20(small).pdf |date=18 December 1958 |publisher=Rocketdyne }}
* {{cite web |first=Ed |last=Kyle |title=King of Gods: The Jupiter Missile Story |date=14 August 2011 |website=Space Launch Report |url=http://www.spacelaunchreport.com/jupiter.html|archive-url=https://web.archive.org/web/20110702094020/http://www.spacelaunchreport.com/jupiter.html|url-status=usurped|archive-date=2 July 2011}}
* {{cite book |first=Donald |last=Mackenzie |title=Inventing Accuracy, a Historical Sociology of Nuclear Missile Guidance |url=https://archive.org/details/inventingaccurac00dona |url-access=registration |date=1993 |publisher=MIT Press }}
*{{cite book |first=Jacob |last=Neufeld |title=The development of ballistic missiles in the United States Air Force 1945–1960 |publisher=DIANE Publishing |isbn=9781428992993 |date=1990 }}
* {{cite book |last1=Walker |first1=James |first2=Lewis |last2=Bernstein |first3=Sharon |last3=Lang |title=Seize the High Ground: The U. S. Army in Space and Missile Defense |publisher=Center of Military History |location=Washington, D.C. |url=https://archive.org/details/seizehighgroundt00wash |access-date=13 May 2013 |year=2003 |isbn=9780160723087 |oclc=57711369 |df=dmy-all |url-access=registration }}

==External links==
{{Commons category|Jupiter (missile)}}
* [https://web.archive.org/web/20040603144659/http://www.redstone.army.mil/history/systems/jupiter/chapter1.html Jupiter IRBM History], U.S. Army – Redstone Arsenal
* [https://web.archive.org/web/20111010114842/http://astronautix.com/lvs/jupiter.htm Jupiter IRBM], Encyclopedia Astronautica
* [https://web.archive.org/web/20131113182651/http://www.hlswilliwaw.com/Jupiters/index.htm The Jupiter Missiles of Turkey], G. L. Smith
* [https://web.archive.org/web/20161228053143/http://astronautix.com/j/jupitera.html Jupiter-A at Astronautix.com]
* [http://basilicatatopsecret.altervista.org/ Jupiter in Italy]
* [https://jupiter.skeetv.net/ Jupiter SM-78]

{{US missiles}}
{{USAF missiles}}
{{Project Mercury}}
{{USAF system codes}}
{{Authority control}}

{{DEFAULTSORT:Pgm-019}}
[[Category:1957 in spaceflight]]
[[Category:1958 in spaceflight]]
[[Category:1959 in spaceflight]]
[[Category:1960 in spaceflight]]
[[Category:1961 in spaceflight]]
[[Category:Cold War missiles of the United States]]
[[Category:Medium-range ballistic missiles of the United States]]
[[Category:Nuclear missiles of the United States]]
[[Category:Space launch vehicles of the United States]]
[[Category:Theatre ballistic missiles]]
[[Category:Military equipment introduced in the 1950s]]