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up. Launch crews initially did nothing as they reasoned that the Earth's rotation would gradually take it away from land and they wished to continue collecting data as long as possible. Eventually though, they became nervous about it exploding or pitching over, so the destruct command was sent around 50 seconds into launch. High-altitude wind caused debris to land in the town of Orcutt near the base. After Thor 203 repeated the same failure four weeks later, an investigation found that the culprit was a safety wire that had been meant to prevent the control tape in the programmer from inadvertently coming loose during vehicle assembly. The wire would ordinarily be cut after installation of the programmer in the missile, but
Douglas technicians had forgotten this important step, thus the tape could not be spooled and the pitch and roll sequence did not activate. Another 23 Thor missile tests were carried out during 1959, with only one failure, when Missile 185 on 16 December, the second RAF launch, broke up due to a control malfunction.
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facilities were not designed for a full duration firing. Missile 107 had not been given a PFRF at all and its launch ended in a pad explosion. A static firing stand for Thor tests was only opened in May 1958, at which point the missile's launch record stood at four successes and nine failures, including four launchpad explosions. For comparison, at the end of May 1958 Jupiter had five successes and three failures with no pad explosions. Thanks to the thorough testing done at
Huntsville, Jupiter missiles mostly all arrived at CCAS in flight-ready condition while Thors typically required extensive repairs or modification before launch.
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a long shed mounted on steel rails, then used a powerful hydraulic launcher-erector to lift the missile to an upright position for launch. Once it was standing on the launch mount, the missile was fueled and could be fired. The entire launch sequence, from starting to roll back the missile shelter through to ignition of the rocket engine and lift-off, took approximately 15 minutes. Main engine burn time was almost 2.5 minutes, boosting the missile to a speed of 14,400 ft/s (4,400 m/s). Ten minutes into its flight the missile reached an altitude of 280 miles (450 km), close to the
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were conducted. Modified bearing retainers were not installed. Subsequently, six consecutive Thor and Atlas launches failed during
February–April 1958, several due to turbopump problems. The following four months did not include any turbopump failures, but the 17 August launch of the world's first lunar probe on Thor-Able 127 ended in an explosion due to a turbopump failure. A month later, Atlas 6B also suffered a turbopump failure and the Air Force gave in and agreed to replace the turbopumps in all of their missiles, after which there were no more launch failures due to a turbopump problem.
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foam at high altitude as the air pressure decreased. The other was that pump shaft vibration from the nearly 10,000 RPM operating speed would cause the bearings to come out of their sockets, resulting in the pump abruptly seizing up. The Army had suspended
Jupiter launches for four months until the turbopump issues could be resolved, and as a result no more pump failures affected that program.
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failures. The initial Thor tests in 1957 used an early version of the
Rocketdyne LR-79 engine with a conical nozzle and 135,000 lbf (600 kN) of thrust. By early 1958, this had been replaced by an improved model with a bell-shaped nozzle see and 150,000 lbf (670 kN) of thrust. The fully developed Thor IRBM had 162,000 lbf (720 kN) of thrust.
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January 1957. The engine lost thrust almost immediately after liftoff, and the Thor fell onto the launch pad and exploded. A film of prelaunch preparations showed crews dragging a liquid oxygen (LOX) filler hose through a sandy area, which led to the belief that debris entering the LOX, caused the failure of a valve.
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Institute for
Atmospheric Physics investigated the phenomena and linked it to the Thor rocket launch after contacting military personnel at Vandenberg Air Force Base. When the launch records were later declassified, the United States Air Force released a memo explaining that the cloud was "the result
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All 60 of the Thor missiles deployed in the UK were based at above-ground launch sites. The missiles were stored horizontally on transporter-erector trailers and covered by a retractable missile shelter. To fire the weapon, the crew used an electric motor to roll back the missile shelter, essentially
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Five successful Thor tests were conducted in June–July 1958, the last one carrying a mouse named Wickie on a biological mission; the capsule sank into the ocean and could not be recovered. Thor 126 (26 July) lost thrust 50 seconds into launch when a LOX valve inadvertently closed. The vehicle pitched
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The
Jupiter, Thor, and Atlas missiles all used a variant of the Rocketdyne LR-79 engine and all three suffered launch failures due to a marginal turbopump design. There were two separate problems with the pumps. The first was the discovery during testing at Huntsville that the lubricant oil tended to
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Thor 102 was launched on 20 April. The booster performed normally, but the flight was terminated at 35 seconds after an erroneous console readout caused the Range Safety
Officer to believe that the missile was headed inland instead of out to sea. The tracking console was found to be wired in reverse.
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The third Thor launch (Missile 103) exploded four minutes before the planned launch after a defective valve allowed LOX tank pressure to build up to unsafe levels. The responsible technicians had also failed to pay attention to the tank pressure gauges. LC-17B consequently had to be repaired for the
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After a run of successful launches during the first half of 1959, Missile 191, the first to be launched by a Royal Air Force crew, suffered another control malfunction while being launched from VAFB. This time, the missile's pitch and roll program failed to activate and it continued flying straight
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well on its way to operational status, Thor and
Jupiter became obsolete, although both remained in service as missiles until 1963. In retrospect, the IRBM program was a poorly conceived idea as it depended on the cooperation of NATO allies, most of whom were not willing to have nuclear missiles on
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The
Jupiter program was more successful due to far better testing and preparation, with each missile given a full duration static firing in Huntsville prior to delivery. Thors were given a PFRF (Pre Flight Readiness Firing) prior to launch; these were between 5 and 15 seconds only as the launching
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With two IRBMs of nearly identical capabilities, it seemed obvious that only one of the two would ultimately achieve operational status, resulting in a competition between the Army and Air Force. Jupiter's testing program began two months after Thor's and proceeded more smoothly. Accidents such as
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The operational variant of the Thor, the DM-18A, began testing in the autumn of 1958, but Missile 138 (5 November) went out of control shortly after liftoff and had to be destroyed. Nonetheless, Thor was declared operational and testing now began at Vandenberg Air Force Base on the West Coast when
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In contrast, the USAF's General Schreiver rejected the idea of sending Thor and Atlas missiles back to the factory so as to not delay the testing program. Instead, in-field modifications to pressurize the turbopump gearboxes and use an oil with a different viscosity that was less prone to foaming
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After the Soviet launches of Sputnik 1 and 2 in late 1957, US Secretary of Defense Charles Wilson announced that both Thor and Jupiter would go into service as his final act before leaving office. This was both out of fear of Soviet capabilities and also to avoid political repercussions from the
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with a ballistic missile. This led to the Jupiter's squat shape, which allowed it to be stored within the confines of a submarine hull. However, the Navy was always concerned about the extremely risky situation of a liquid-fueled rocket stored in the confines of a submarine. By 1956, the Polaris
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The final three Thor tests during 1957 were all successful. 1958 began with back-to-back failures. Thor 114 was destroyed by Range Safety 150 seconds into launch when the guidance system lost power and Thor 120's engine shut down slightly under two minutes after liftoff. The telemetry system had
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Missile 101, the first flight-ready Thor, arrived at Cape Canaveral in October 1956. It was erected at LC-17B and underwent several practice propellant loading/unloading exercises, a static firing test, and a month-long delay while a defective relay was replaced. Launch finally took place on 25
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Missile 104, launched 22 August from the newly opened LC-17A, broke up at T+92 seconds due to a drop in signal strength from the programmer, causing the engine to gimbal hard right. The guidance system tried to compensate, but the resulting structural loads exceeded the strength of the missile
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Engine component tests began in March 1956. The first engineering model engine was available in June, followed by the first flight engine in September. Early Thor engines suffered from foaming turbopump lubricating oil at high altitudes and bearing retention issues, resulting in several launch
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On February 28, 1963, a Thor rocket carrying a spy satellite into orbit was launched from Vandenberg Airforce Base. The rocket went off course and mission control detonated the rocket at an altitude of 27 mi (44 km) before it could reach orbit. The rocket detonation produced a large
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circular cloud that appeared over the southwestern United States. Due to its mysterious nature, appearing at a very high altitude and being visible for hundreds of miles, the cloud attracted widespread attention and was published by the news media. The cloud was featured on the cover of
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would deploy a long-range ballistic missile before the U.S., in January 1956 the USAF began developing the Thor, a 1,500-mile (2,400 km) intermediate-range ballistic missile. The program proceeded quickly as a stop-gap measure, and within three years of inception the first of 20
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Thor 105 (20 September) completed the first successful flight, which occurred 21 months after the start of the program. No telemetry equipment was included on this missile, with the resulting mass savings allowing a total range of 1,500 miles (2,400 km).
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Launch Emplacement One (LE1) after a Thor missile launch failure and explosion contaminated the island with plutonium during the Operation "Bluegill Prime" nuclear test, July 1962. The retractable missile shelter (on rails) can be seen at the
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rocket well on its way to operational status, both Thor and Jupiter programs became obsolete as delivery vehicles, yet continued to be built and deployed until 1963 for political reasons and to maintain aerospace industry employment.
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8 July 1962, Thor missile 195 launched a Mk4 reentry vehicle containing a W49 thermonuclear warhead to an altitude of 250 miles (400 km). The warhead detonated with a yield of 1.45 Mt of TNT (6.07 PJ). This was the
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launch failed six months later due to a seized turbopump, it was concluded that a similar failure had occurred on 108. However, 108 did not have sufficient instrumentation to determine the exact nature of the failure.
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277:, the Thor could be carried by the USAF's cargo aircraft of the time, which made its deployment more rapid. The launch facilities were not transportable and had to be built on site. Once the first generation of
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400:. The missile was to use existing technology, skills, abilities, and techniques to speed entry into service. On 27 December 1955, Douglas was awarded the prime contract for the airframe and integration. The
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Development of the Thor was initiated by the USAF in 1954. The goal was a missile system that could deliver a nuclear warhead over a distance of 1,150 to 2,300 miles (1,850 to 3,700 km) with a
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in the Pacific Ocean and had the ability to destroy satellites in low Earth orbit. With prior warning of an impending launch, they could destroy a Soviet spy satellite soon after orbital insertion.
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580:, was originally designed to attack high-value targets like airfields, train switching yards and command and control sites with extremely high accuracy. The Redstone team, under the direction of
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Missile 151 flew successfully on 16 December. On 30 December, a near repeat performance of the 5 November failure happened when Missile 149 lost control and was destroyed 40 seconds into launch.
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the nose cone/reentry vehicle. Douglas' proposal included choosing bolted tank bulkheads (as opposed to the initially suggested welded ones) and a tapered fuel tank for improved aerodynamics.
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The Thor was initially deployed with a very blunt conical G.E. Mk 2 'heat sink' re-entry vehicle. They were later converted to the slender G.E. Mk 3 ablative RV. Both RVs contained a
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Missile 151, nicknamed "Tune Up", on December 16, 1958, just prior to its launch from Vandenberg Air Force Base. The successful test was conducted a year after the base was activated.
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their soil, and was also surpassed by the ICBM program, yet continued anyway for political reasons and a desire to keep the workforce at their respective assembly plants employed.
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the explosion of Thor 103 were avoided, and the turbopump issues that plagued early Rocketdyne engines were also resolved in Jupiter much earlier than the Air Force's missiles.
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down and broke up from aerodynamic loads. On 30 July, six Douglas technicians were severely burned, three fatally, when a LOX valve failed at the Thor static test stand in
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On 19 April, Missile 121 dropped back onto LC-17B and exploded, putting the pad out of action for three months. A fuel duct collapse was believed to have been the culprit.
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program was proposed instead, which featured a solid-fueled SLBM that was much lighter and safer to store. The Navy quickly switched to Polaris and dropped Jupiter.
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Missile 108 (11 October) exploded around T+140 seconds without prior warning. Engineers were initially unable to determine the cause of the failure. After the first
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separated from the missile fuselage and began its descent toward the target. Total flight time from launch to target impact was approximately 18 minutes.
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booster engine, with removal of one thrust chamber and a rerouting of the plumbing to allow the engine to fit within the smaller Thor thrust section.
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missile saw more use, but both were quickly eclipsed by the Air Force's long range ICBM program, which could be fired from US soil. By 1959, with the
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bunker had to be used to allow the completion of the facility in time, with launchpad LC-17B completed just in time for the first test flight.
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of 2 miles (3.2 km). This range would allow Moscow to be attacked from a launch site in the UK. The initial design studies were headed by
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based in the US became operational, Thor missiles were quickly retired. The last of the missiles was withdrawn from operational alert in 1963.
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The first generation of Thor missiles were rushed into service, and design mistakes resulted in a 24% launch failure rate. The competing
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Phase II testing with the AC Spark Plug inertial guidance system began 7 December with the first successful flight on 19 December 1957.
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Thor's lasting legacy was not as a missile, but its use as the basis for the Thor/Delta space launcher family into the 21st century.
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accepted the offer to have Thor missiles stationed on their soil. Italy and Turkey both agreed to accept Jupiter missiles. Thor was
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Despite being retired from deployment as a missile a few years after deployment, the Thor rocket found widespread use as a space
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flight, Thor and nuclear device destroyed 59 seconds after launch at 30,000 to 35,000 feet (9,100 to 10,700 m) altitude.
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Melissen, Jan. "The Thor saga: Anglo‐American nuclear relations, US IRBM development and deployment in Britain, 1955–1959."
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was based on mostly new technology, unlike the Delta II. The last rocket of the Delta rocket family flew on 9 April 2024.
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RAF Squadrons, a Comprehensive record of the Movement and Equipment of all RAF Squadrons and their Antecedents since 1912
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experienced a power failure during launch, so the reason for the engine cutoff could not be satisfactorily determined.
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for roll control flanking the main engine, similar to the Atlas vernier engines on the sides of the propellant tanks.
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Missile 107 (3 October) fell back onto LC-17A and exploded at launch when a gas generator valve failed to open.
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Family: Thor IRBM, Thor DM-18 (single stage LV); Thor DM-19 (rocket 1st stage), Thor DM-21 (rocket 1st stage),
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Deployment of the IRBM fleet to Europe proved more difficult than expected, as no NATO members other than the
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workplace layoffs that would result at either Douglas or Chrysler if one of the two missiles were canceled.
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The IRBM program was quickly eclipsed by the Air Force's ICBM program and made redundant. By 1959, with
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in 1958, with the remaining units becoming active in 1959. All were deactivated by September 1963.
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flight, Thor and nuclear device destroyed on launch pad, which was contaminated with plutonium.
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used boosters derived from the initial Thor missile, and continued on into the 21st century.
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8 ft (2.4 m) diameter, 65 ft (20 m) long (so it could be carried by
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Inertial guidance system with radio backup (for low susceptibility to enemy disruption)
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Thor squadrons became operational in the UK. The UK deployment carried the codename '
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The Thor IRBM: The Cuan Missile Crisis and the subsequent run-down of the Thor Force
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RAF Strategic Nuclear Deterrent Forces, their Origins, Roles and Deployment 1946–69
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Defense Nuclear Agency. Operation Dominic I. 1962. Report DNA 6040F. Page 229-241.
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On 30 November 1955, three companies were given one week to bid on the project:
225:. Thor was 65 feet (20 m) in height and 8 feet (2.4 m) in diameter.
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1729:. Shrewsbury, Shropshire, UK: Airlife Publishing, 1988 (second edition 2001).
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Magazine in May 1963, and had a full page image published in the May issue of
217:. It was deployed in the United Kingdom between 1959 and September 1963 as an
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operated a maximum of 60 missiles, with each squadron controlling 3 missiles
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4468:
4228:
4212:
4192:
4182:
4172:
4133:
4083:
4073:
4026:
3960:
3930:
3890:
3875:
3712:
3665:
3618:
3593:
3558:
3478:
3367:
3285:
3198:
3100:
2944:
2939:
2904:
2848:
2838:
2833:
2828:
2823:
2818:
2813:
2304:
2284:
2096:
1911:
1672:
Thor Ballistic Missile: The United States and United Kingdom in Partnership
1121:
1021:
930:
917:
904:
891:
878:
874:
662:
364:
340:
324:
261:
7004:
6999:
6944:
6889:
6594:
6366:
5293:
5039:
4888:
4760:
4720:
4491:
4486:
4463:
3900:
3670:
3660:
3563:
3351:
3300:
3265:
3250:
3225:
3060:
2984:
2959:
2929:
2909:
2894:
2808:
2503:
2269:
2264:
2259:
2249:
1906:
1891:
1798:
1607:
1173:
983:
970:
926:
900:
692:
328:
289:
1631:
Prospero, Journal of the British Rocketry Oral History Programme (BROHP)
500:, lost thrust and broke up at T+146 seconds due to a turbopump failure.
6701:
6514:
5930:
5908:
5654:
4755:
4750:
3702:
3603:
3573:
3085:
3075:
3065:
3009:
3004:
2676:
2025:
2020:
2015:
2010:
2005:
2000:
1901:
1896:
1886:
1574:, Vandenberg AFB, California: Department of the Air Force, pp. 1–2
1407:
1402:
1165:
524:
401:
712:
flight, tracking lost after launch, Thor and nuclear device destroyed.
6604:
6556:
6324:
4928:
4284:
3498:
3447:
2319:
2066:
2040:
1876:
1397:
1060:
1000:
987:
974:
961:
948:
596:
595:
became involved in the Jupiter program, with the objective of arming
482:
463:
The short flight raised confidence that Thor could fly successfully.
409:
404:
division of North American Aviation was awarded the engine contract,
308:
435:
374:
10,000 mph (4.5 km/s) maximum speed during warhead reentry
4147:
2686:
2071:
2061:
2045:
2035:
2030:
803:
792:
788:
654:
569:
332:
304:
284:
A small number of Thors with "Thrust Augmented Delta" boosters and
3127:
United States tri-service missile and drone designations post-1962
783:. It was the first in a large family of space launch vehicles—the
7102:
7097:
6649:
6122:
4031:
3905:
3895:
3820:
3753:
2999:
2681:
2666:
2472:
2467:
1984:
1979:
1974:
1969:
1964:
1954:
1949:
1944:
1939:
1934:
1778:
1095:
1077:
1051:
1038:
1025:
592:
1788:
6275:
4745:
4635:
4113:
4093:
3955:
3915:
3815:
3680:
3655:
3628:
3533:
2949:
2645:
2608:
1794:"YouTube contemporary film of Thor missiles at North Pickenham"
787:
rockets. The last remaining direct descendant of the Thor, the
670:
451:. The compressed development schedule meant that plans for the
1627:
Project Emily: The Thor IRBM and the Royal Air Force 1959–1963
6984:
5721:
4309:
4259:
4254:
3357:
3295:
3290:
2603:
2598:
1691:
To Reach The High Frontier: A History of U.S. Launch Vehicles
354:
1487:"Locks on nuclear missiles changed after launch key blunder"
1455:
Nuclear Weapons of the United States, An Illustrated History
273:'. One of the advantages of the design was that, unlike the
32:
6989:
2593:
2588:
2578:
2558:
2523:
1237:
288:
remained operational in the anti-satellite missile role as
214:
7414:
Intermediate-range ballistic missiles of the United States
4425:
1251:
Specific Impulse (sea level): 248 seconds (2.43 km/s)
360:
A gross takeoff weight of 110,000 lb (50,000 kg)
2106:
1457:, pp. 167–168, Schiffer Publishing Ltd., Atglen, PA, 1996
1281:
681:
285:
4379:
United States tri-service rocket designations post-1963
1430:"Thor Missile Deployment in the UK | Harrington Museum"
642:
588:
that was accurate to about 5,900 feet (1,800 m).
7332:
1473:. Air Historical Branch, Royal Air Force. p. 50.
649:
starting in August 1958, operated by 20 squadrons of
1784:
UK Thor missile launch sites on Secret Bases website
543:
Thor missile 187 test. Cape Canaveral, May 12, 1959.
343:). They refined the specifications to an IRBM with:
3169:
1963 United States Tri-Service missile designations
1242:
Liftoff Thrust (sl): 150,000 lbf (670 kN)
1536:. Vol. 140, no. 3564. pp. 292–294.
1485:
1693:. Lexington: University Press of Kentucky, 2002.
1216:Maximum speed: 11,000 mph (17,700 km/h)
673:of its elliptical flight path. At that point the
7380:
1584:
1569:
1527:
1207:Range: 1,500–1,900 mi (2,400–3,000 km)
419:The engine was a direct descendant of the Atlas
765:of a military operation", but did not clarify.
563:
292:until April 1975. These missiles were based on
1689:. In Roger Launius and Dennis Jenkins (Eds.),
1373:List of military aircraft of the United States
1335:Flyaway Unit Cost: US$ 750,000 in 1958 dollars
1248:Specific Impulse: 282 seconds (2.77 km/s)
240:The missile's lasting legacy continued as the
4411:
3153:
2770:
1814:
1266:Chamber Pressure: 590 psi (4.1 MPa)
702:
496:On 22 April, Missile 117, carrying the first
1719:
1245:Thrust (vac): 170,000 lbf (760 kN)
363:Propulsion provided by half of the existing
146:49,590 kilograms (109,330 lb) at start.
37:A Thor intermediate range ballistic missile.
1789:Maxwell Hunter, "Father of the Thor Rocket"
1708:. New York: Duell, Sloan, and Pearce, 1961.
1530:"Stratospheric Cloud Over Northern Arizona"
1483:
1159:
7424:Military equipment introduced in the 1950s
4418:
4404:
3160:
3146:
2777:
2763:
1828:
1821:
1807:
1332:Recurring Price US dollars: $ 6.25 million
1329:Development Cost US dollars: $ 500 million
1434:Harrington Aviation Museum | CarpetBagger
1257:Mass Engine: 1,418 lb (643 kg)
1204:Core Diameter: 8.0 ft (2.44 m)
802:
625:
546:
538:
523:
434:
430:
303:
807:Map with former PGM-17 operators in red
568:The Jupiter missile, a joint effort of
7404:Cold War missiles of the United States
7381:
1587:"Cloud Ring In The Upper Stratosphere"
439:Thor 101 on a launch pad, January 1957
412:the backup radio guidance system, and
408:the primary inertial guidance system,
299:
4399:
3141:
2758:
1802:
1706:The Mighty Thor: Missile in Readiness
742:
154:19.76 metres (64 ft 10 in).
7409:Nuclear weapons of the United States
1638:Project Emily: Thor IRBM and the RAF
1570:Jackson, Jeff G. (26 January 1995),
1498:from the original on 12 January 2022
1466:
1296:equivalent to 1.44 Megatons of
1140:No. 254 (Strategic Missile) Squadron
1127:No. 218 (Strategic Missile) Squadron
1114:No. 223 (Strategic Missile) Squadron
1101:No. 130 (Strategic Missile) Squadron
1088:No. 144 (Strategic Missile) Squadron
1070:No. 220 (Strategic Missile) Squadron
1057:No. 113 (Strategic Missile) Squadron
1044:No. 107 (Strategic Missile) Squadron
993:No. 240 (Strategic Missile) Squadron
980:No. 226 (Strategic Missile) Squadron
967:No. 150 (Strategic Missile) Squadron
954:No. 102 (Strategic Missile) Squadron
923:No. 269 (Strategic Missile) Squadron
910:No. 142 (Strategic Missile) Squadron
897:No. 106 (Strategic Missile) Squadron
884:No. 104 (Strategic Missile) Squadron
519:
219:intermediate-range ballistic missile
47:Intermediate-range ballistic missile
18:Intermediate-range ballistic missile
1779:History of the Delta Launch Vehicle
1260:Diameter: 8.0 ft (2.44 m)
1226:; 1,000 lbf (4.4 kN) each
1031:No. 82 (Strategic Missile) Squadron
1018:No. 77 (Strategic Missile) Squadron
941:No. 98 (Strategic Missile) Squadron
871:No. 97 (Strategic Missile) Squadron
798:
657:control. The first active unit was
13:
1657:Royal Air Force Historical Society
1619:
1528:MacDonald, James (19 April 1963).
1347:First Launch Date: 25 January 1957
1229:Rocketdyne LR79-NA-9 (Model S-3D);
1210:Ceiling: 300 mi (480 km)
347:A 1,750-mile (2,820 km) range
14:
7435:
4385:Drones designated in UAV sequence
3122:USAF missile designations 1947–51
1761:
1585:MacDonald, James (15 June 1963).
1350:Last Launch Date: 5 November 1975
768:
313:Cape Canaveral Space Force Museum
119:About 225; peak deployment was 60
7366:
7354:
7342:
2119:
1284:warhead on Mk. 2 reentry vehicle
1195:109,800 lb (49,800 kg)
835:
813:
684:with an explosive yield of 1.44
187:2,820 kilometres (1,750 mi)
31:
3794:BGM-109/AGM-109/RGM-109/UGM-109
3106:Supersonic Low Altitude Missile
2789:rocket and missile designations
1600:
791:, was retired in 2018, and the
760:. Prof. James MacDonald at the
213:(USAF). It was named after the
1770:from Encyclopedia Astronautica
1578:
1563:
1548:
1542:10.1126/science.140.3564.292.b
1521:
1510:
1477:
1460:
1447:
1422:
1272:Thrust to Weight Ratio: 120.32
113:
1:
1484:Sam Marsden (1 August 2013).
1415:
1290:2,200 lb (1,000 kg)
1201:6,889 lb (3,125 kg)
1168:(suborbital launch vehicle),
727:event of nuclear test series
615:
195:630 kilometres (390 mi).
1713:Journal of Strategic Studies
1383:List of Thor DM-18A launches
630:Thor missile T-110 (left of
564:Service rivalry with Jupiter
467:second time in four months.
449:Cape Canaveral Missile Annex
443:Thor was test launched from
7:
1640:. Tempus Publishing, 2008.
1354:
1323:Total Production Built: 160
1320:Total Development Built: 64
1183:65.0 ft (19.82 m)
333:Ramo-Wooldridge Corporation
10:
7440:
7419:Theatre ballistic missiles
1559:. 14 May 1963. p. 73.
1176:(orbital launch vehicle).
1172:(anti-ballistic missile),
772:
703:Nuclear-armed test flights
682:W-49 thermonuclear warhead
632:English Electric Lightning
619:
584:, ultimately delivered an
255:
175:kerosene and liquid oxygen
7323:
7272:
7136:
7055:
6294:
6153:
5276:
4977:
4776:
4434:
4368:
4242:
4221:
4014:
3746:
3466:
3176:
3114:
3053:
2882:
2862:
2801:
2794:
2699:
2659:
2628:
2621:
2551:
2486:
2438:
2431:
2415:
2364:
2357:
2242:
2204:
2186:
2163:
2135:
2128:
2117:
2089:
2054:
1993:
1927:
1920:
1864:
1857:
1834:
1720:Books referencing RAF use
1470:The Bomber Role 1945–1970
1189:9.0 ft (2.74 m)
191:
179:
171:
166:
158:
150:
142:
137:
123:
112:
104:
94:
86:
81:
65:
60:
53:Place of origin
52:
42:
30:
23:
1687:Delta: The Ultimate Thor
1674:. Fonthill Media, 2015.
1659:. Journal 42, May 2008.
1160:Specifications (PGM-17A)
591:During development, the
586:inertial guidance system
205:was the first operative
99:Douglas Aircraft Company
77:(operational deployment)
7325:Unknown or not assigned
4427:United States Air Force
2787:United States Air Force
1572:30th Space Wing History
1467:Wynn, Humphrey (1984).
1317:Total Number Built: 224
1306:0.6 mi (1 km)
829:United States Air Force
398:North American Aviation
211:United States Air Force
162:2.4 metres (8 ft).
70:United States Air Force
2651:United Launch Alliance
1829:Thor and Delta rockets
1774:Thor IRBM History site
808:
638:
556:
544:
529:
514:Sacramento, California
440:
316:
223:thermonuclear warheads
4355:M30 GMLRS/M31 GMLRS-U
1715:15#2 (1992): 172-207.
1388:Strategic Air Command
1254:Burn time: 165 s
1084:North Luffenham Wing
806:
762:University of Arizona
734:25 July 1962, failed
715:19 June 1962, failed
629:
550:
542:
527:
438:
431:Phase I test launches
307:
3639:AGM-84/RGM-84/UGM-84
2340:Shepherds Grove
2330:North Pickenham
2325:North Luffenham
1393:Thor (rocket family)
1344:Success Rate: 76.27%
775:Thor (rocket family)
708:2 June 1962, failed
215:Norse god of thunder
7399:1963 in spaceflight
7394:1961 in spaceflight
7389:1960 in spaceflight
2795:Air-to-air missiles
2423:Common Booster Core
2315:Melton Mowbray
1224:Rocketdyne LR101-NA
1092:RAF North Luffenham
1074:RAF North Pickenham
1035:RAF Shepherds Grove
659:No. 77 Squadron RAF
578:Huntsville, Alabama
329:Dr. Adolph K. Thiel
300:Initial development
286:W-49 Mod 6 warheads
25:SM-75/PGM-17A Thor
7349:Nuclear technology
3054:Undesignated types
2863:1961–1963 sequence
2802:1955–1961 sequence
2310:Ludford Magna
2275:Coleby Grange
1685:Forsyth, Kevin S.
1633:No 4, Spring 2007.
1596:. pp. 99–148.
1311:First Flight: 1958
1213:Guidance: Inertial
1144:RAF Melton Mowbray
809:
743:1963 mystery cloud
729:Operation Fishbowl
651:RAF Bomber Command
647:deployed to the UK
639:
636:RAF Museum Cosford
557:
545:
530:
441:
339:and previously of
325:Cmdr. Robert Truax
317:
248:families of space
132:Thor rocket family
82:Production history
7330:
7329:
4393:
4392:
3135:
3134:
2878:
2877:
2752:
2751:
2695:
2694:
2641:McDonnell Douglas
2617:
2616:
2547:
2546:
2353:
2352:
2115:
2114:
2085:
2084:
1680:978-1-78155-481-4
1646:978-0-7524-4611-0
1555:"Mystery Cloud".
1453:James N. Gibson,
1314:Last Flight: 1980
914:RAF Coleby Grange
888:RAF Ludford Magna
582:Wernher von Braun
520:Phase II launches
260:Fearful that the
207:ballistic missile
199:
198:
7431:
7371:
7370:
7369:
7359:
7358:
7357:
7347:
7346:
7345:
7338:
7311:
7301:
7296:
7291:
7281:
7265:
7255:
7245:
7235:
7225:
7220:
7215:
7210:
7205:
7195:
7180:
7175:
7170:
7150:
7145:
7129:
7119:
7109:
7089:
7084:
7079:
7074:
7064:
7048:
7043:
7038:
7033:
6973:
6963:
6933:
6928:
6898:
6873:
6843:
6838:
6833:
6818:
6798:
6788:
6738:
6733:
6718:
6713:
6708:
6678:
6673:
6588:
6583:
6578:
6573:
6538:
6533:
6498:
6493:
6488:
6483:
6473:
6428:
6418:
6408:
6398:
6393:
6388:
6383:
6373:
6287:
6267:
6247:
6237:
6217:
6197:
6187:
6177:
6167:
6041:
5922:
5885:
5768:
5753:
5718:
5713:
5683:
5503:
5486:
5367:
5362:
5352:
5322:
5249:
5229:
5209:
5204:
5199:
5194:
5189:
5116:
5106:
5096:
5061:
5056:
5051:
5046:
5011:
5006:
4991:
4965:
4955:
4945:
4935:
4925:
4895:
4875:
4855:
4845:
4835:
4815:
4737:
4727:
4707:
4702:
4692:
4647:
4540:
4535:
4530:
4525:
4515:
4505:
4500:
4480:
4420:
4413:
4406:
4397:
4396:
4380:
3162:
3155:
3148:
3139:
3138:
2799:
2798:
2779:
2772:
2765:
2756:
2755:
2626:
2625:
2436:
2435:
2362:
2361:
2295:Full Sutton
2133:
2132:
2123:
1925:
1924:
1862:
1861:
1823:
1816:
1809:
1800:
1799:
1740:Wynn, Humphrey.
1612:
1611:
1604:
1598:
1597:
1591:
1582:
1576:
1575:
1567:
1561:
1560:
1552:
1546:
1545:
1534:Science Magazine
1525:
1519:
1514:
1508:
1507:
1505:
1503:
1489:
1481:
1475:
1474:
1464:
1458:
1451:
1445:
1444:
1442:
1440:
1426:
1378:List of missiles
1269:Area Ratio: 8.00
1135:Northamptonshire
1109:Northamptonshire
841:
839:
838:
819:
817:
816:
799:Former operators
750:Science Magazine
574:Redstone Arsenal
498:Able upper stage
414:General Electric
337:Redstone Arsenal
115:
35:
26:
21:
20:
7439:
7438:
7434:
7433:
7432:
7430:
7429:
7428:
7379:
7378:
7377:
7367:
7365:
7355:
7353:
7343:
7341:
7333:
7331:
7326:
7319:
7309:
7299:
7294:
7289:
7279:
7268:
7263:
7253:
7243:
7233:
7223:
7218:
7213:
7208:
7203:
7193:
7178:
7173:
7168:
7148:
7143:
7132:
7127:
7117:
7107:
7087:
7082:
7077:
7072:
7062:
7051:
7046:
7041:
7036:
7031:
6971:
6961:
6931:
6926:
6896:
6871:
6841:
6836:
6831:
6816:
6796:
6786:
6736:
6731:
6716:
6711:
6706:
6676:
6671:
6586:
6581:
6576:
6571:
6536:
6531:
6496:
6491:
6486:
6481:
6471:
6426:
6416:
6406:
6396:
6391:
6386:
6381:
6371:
6290:
6285:
6265:
6245:
6235:
6215:
6195:
6185:
6175:
6165:
6149:
6039:
5920:
5883:
5766:
5751:
5716:
5711:
5681:
5501:
5484:
5365:
5360:
5350:
5320:
5272:
5247:
5227:
5207:
5202:
5197:
5192:
5187:
5114:
5104:
5094:
5059:
5054:
5049:
5044:
5009:
5004:
4989:
4973:
4963:
4953:
4943:
4933:
4923:
4893:
4873:
4853:
4843:
4833:
4813:
4772:
4735:
4725:
4705:
4700:
4690:
4645:
4538:
4533:
4528:
4523:
4513:
4503:
4498:
4478:
4430:
4424:
4394:
4389:
4378:
4364:
4238:
4217:
4010:
3881:RUM-125/UUM-125
3861:CQM-121/CGM-121
3742:
3462:
3172:
3166:
3136:
3131:
3110:
3049:
2874:
2858:
2790:
2783:
2753:
2748:
2691:
2655:
2613:
2543:
2482:
2427:
2411:
2349:
2238:
2200:
2182:
2159:
2124:
2111:
2081:
2050:
1989:
1916:
1853:
1830:
1827:
1764:
1759:
1722:
1704:Hartt, Julian.
1622:
1620:Further reading
1616:
1615:
1606:
1605:
1601:
1589:
1583:
1579:
1568:
1564:
1554:
1553:
1549:
1526:
1522:
1515:
1511:
1501:
1499:
1492:Daily Telegraph
1482:
1478:
1465:
1461:
1452:
1448:
1438:
1436:
1428:
1427:
1423:
1418:
1357:
1181:Overall length:
1162:
958:RAF Full Sutton
937:Driffield Wing
851:Royal Air Force
836:
834:
814:
812:
801:
777:
771:
752:in April 1963,
745:
705:
675:reentry vehicle
624:
618:
566:
552:Johnston Island
522:
433:
383:vernier engines
302:
294:Johnston Island
267:Royal Air Force
258:
250:launch vehicles
192:Flight altitude
184:
182:
167:
130:
75:Royal Air Force
73:
61:Service history
38:
24:
19:
12:
11:
5:
7437:
7427:
7426:
7421:
7416:
7411:
7406:
7401:
7396:
7391:
7376:
7375:
7363:
7361:United Kingdom
7351:
7328:
7327:
7324:
7321:
7320:
7318:
7317:
7312:
7307:
7302:
7297:
7292:
7287:
7282:
7276:
7274:
7270:
7269:
7267:
7266:
7261:
7256:
7251:
7246:
7241:
7236:
7231:
7226:
7221:
7216:
7211:
7206:
7201:
7196:
7191:
7186:
7181:
7176:
7171:
7166:
7165:
7164:
7159:
7151:
7146:
7140:
7138:
7134:
7133:
7131:
7130:
7125:
7120:
7115:
7110:
7105:
7100:
7095:
7090:
7085:
7080:
7075:
7070:
7065:
7059:
7057:
7053:
7052:
7050:
7049:
7044:
7039:
7034:
7029:
7028:
7027:
7022:
7017:
7012:
7007:
7002:
6997:
6992:
6987:
6982:
6974:
6969:
6964:
6959:
6958:
6957:
6952:
6947:
6939:
6934:
6929:
6924:
6923:
6922:
6917:
6909:
6904:
6899:
6894:
6893:
6892:
6887:
6882:
6874:
6869:
6868:
6867:
6862:
6854:
6849:
6844:
6839:
6834:
6829:
6824:
6819:
6814:
6813:
6812:
6807:
6799:
6794:
6789:
6784:
6779:
6774:
6773:
6772:
6767:
6759:
6758:
6757:
6752:
6744:
6739:
6734:
6729:
6724:
6719:
6714:
6709:
6704:
6699:
6698:
6697:
6692:
6687:
6679:
6674:
6669:
6664:
6659:
6654:
6653:
6652:
6647:
6642:
6637:
6632:
6627:
6622:
6617:
6609:
6608:
6607:
6602:
6597:
6589:
6584:
6579:
6574:
6569:
6564:
6559:
6554:
6549:
6544:
6539:
6534:
6529:
6524:
6523:
6522:
6517:
6509:
6504:
6499:
6494:
6489:
6484:
6479:
6474:
6469:
6464:
6459:
6454:
6449:
6448:
6447:
6442:
6434:
6429:
6424:
6419:
6414:
6409:
6404:
6399:
6394:
6389:
6384:
6379:
6374:
6369:
6364:
6359:
6354:
6349:
6348:
6347:
6342:
6334:
6333:
6332:
6327:
6319:
6318:
6317:
6312:
6304:
6298:
6296:
6292:
6291:
6289:
6288:
6283:
6278:
6273:
6268:
6263:
6262:
6261:
6256:
6248:
6243:
6238:
6233:
6232:
6231:
6226:
6218:
6213:
6212:
6211:
6206:
6198:
6193:
6188:
6183:
6178:
6173:
6168:
6163:
6157:
6155:
6151:
6150:
6148:
6147:
6146:
6145:
6140:
6135:
6127:
6126:
6125:
6120:
6115:
6110:
6105:
6097:
6096:
6095:
6090:
6085:
6077:
6072:
6071:
6070:
6065:
6057:
6052:
6047:
6042:
6037:
6036:
6035:
6030:
6022:
6017:
6012:
6007:
6002:
6001:
6000:
5995:
5987:
5986:
5985:
5980:
5975:
5967:
5962:
5961:
5960:
5955:
5950:
5940:
5939:
5938:
5928:
5923:
5918:
5917:
5916:
5911:
5903:
5898:
5897:
5896:
5886:
5881:
5880:
5879:
5874:
5866:
5861:
5856:
5855:
5854:
5849:
5841:
5836:
5831:
5826:
5821:
5816:
5811:
5806:
5801:
5796:
5791:
5790:
5789:
5779:
5774:
5769:
5764:
5759:
5754:
5749:
5744:
5739:
5738:
5737:
5732:
5724:
5719:
5714:
5709:
5704:
5699:
5698:
5697:
5692:
5684:
5679:
5674:
5669:
5668:
5667:
5662:
5657:
5649:
5644:
5639:
5634:
5629:
5624:
5623:
5622:
5617:
5609:
5604:
5599:
5594:
5593:
5592:
5587:
5579:
5574:
5569:
5568:
5567:
5562:
5554:
5553:
5552:
5547:
5539:
5538:
5537:
5532:
5524:
5519:
5514:
5509:
5504:
5499:
5498:
5497:
5487:
5482:
5481:
5480:
5475:
5467:
5462:
5461:
5460:
5455:
5450:
5445:
5440:
5432:
5427:
5426:
5425:
5420:
5412:
5407:
5402:
5401:
5400:
5395:
5385:
5384:
5383:
5378:
5368:
5363:
5358:
5353:
5348:
5343:
5338:
5337:
5336:
5328:
5323:
5318:
5313:
5308:
5307:
5306:
5301:
5296:
5291:
5280:
5278:
5274:
5273:
5271:
5270:
5269:
5268:
5263:
5255:
5250:
5245:
5244:
5243:
5238:
5230:
5225:
5220:
5215:
5210:
5205:
5200:
5195:
5190:
5185:
5184:
5183:
5173:
5172:
5171:
5161:
5160:
5159:
5149:
5144:
5139:
5138:
5137:
5132:
5122:
5117:
5112:
5107:
5102:
5097:
5092:
5087:
5082:
5081:
5080:
5075:
5067:
5062:
5057:
5052:
5047:
5042:
5037:
5032:
5027:
5026:
5025:
5020:
5012:
5007:
5002:
4997:
4992:
4987:
4981:
4979:
4975:
4974:
4972:
4971:
4966:
4961:
4956:
4951:
4946:
4941:
4936:
4931:
4926:
4921:
4920:
4919:
4914:
4906:
4901:
4896:
4891:
4886:
4881:
4876:
4871:
4866:
4861:
4856:
4851:
4846:
4841:
4836:
4831:
4826:
4821:
4816:
4811:
4806:
4805:
4804:
4799:
4794:
4786:
4780:
4778:
4774:
4773:
4771:
4770:
4769:
4768:
4763:
4758:
4753:
4743:
4738:
4733:
4728:
4723:
4718:
4713:
4708:
4703:
4698:
4693:
4688:
4683:
4682:
4681:
4676:
4668:
4663:
4658:
4653:
4648:
4643:
4638:
4633:
4628:
4623:
4618:
4613:
4608:
4607:
4606:
4601:
4596:
4591:
4586:
4576:
4575:
4574:
4569:
4564:
4556:
4555:
4554:
4549:
4541:
4536:
4531:
4526:
4521:
4516:
4511:
4506:
4501:
4496:
4495:
4494:
4489:
4481:
4476:
4471:
4466:
4461:
4456:
4455:
4454:
4444:
4438:
4436:
4432:
4431:
4429:system numbers
4423:
4422:
4415:
4408:
4400:
4391:
4390:
4388:
4387:
4382:
4375:
4369:
4366:
4365:
4363:
4362:
4357:
4352:
4347:
4342:
4337:
4332:
4327:
4322:
4317:
4312:
4307:
4302:
4297:
4292:
4287:
4282:
4277:
4272:
4267:
4265:Common Missile
4262:
4257:
4252:
4246:
4244:
4240:
4239:
4237:
4236:
4231:
4225:
4223:
4219:
4218:
4216:
4215:
4210:
4205:
4200:
4195:
4190:
4185:
4180:
4175:
4170:
4165:
4160:
4155:
4150:
4141:
4136:
4131:
4126:
4121:
4116:
4111:
4106:
4101:
4096:
4091:
4086:
4081:
4076:
4071:
4066:
4065:
4064:
4054:
4049:
4044:
4039:
4034:
4029:
4024:
4018:
4016:
4012:
4011:
4009:
4008:
4003:
3998:
3993:
3988:
3983:
3978:
3973:
3968:
3963:
3958:
3953:
3948:
3943:
3938:
3933:
3928:
3923:
3918:
3913:
3908:
3903:
3898:
3893:
3888:
3883:
3878:
3873:
3868:
3863:
3858:
3853:
3848:
3843:
3838:
3833:
3828:
3823:
3818:
3813:
3808:
3803:
3802:
3801:
3791:
3786:
3781:
3776:
3771:
3766:
3761:
3756:
3750:
3748:
3744:
3743:
3741:
3740:
3735:
3730:
3725:
3720:
3715:
3710:
3705:
3700:
3699:
3698:
3688:
3683:
3678:
3673:
3668:
3663:
3658:
3653:
3652:
3651:
3646:
3636:
3631:
3626:
3621:
3616:
3611:
3606:
3601:
3596:
3591:
3586:
3581:
3576:
3571:
3566:
3561:
3556:
3551:
3546:
3541:
3536:
3531:
3526:
3521:
3516:
3511:
3506:
3501:
3496:
3491:
3486:
3481:
3476:
3470:
3468:
3464:
3463:
3461:
3460:
3455:
3450:
3445:
3440:
3435:
3430:
3425:
3420:
3415:
3410:
3405:
3400:
3395:
3390:
3385:
3380:
3375:
3370:
3365:
3360:
3355:
3345:
3340:
3335:
3330:
3325:
3320:
3319:
3318:
3308:
3303:
3298:
3293:
3288:
3283:
3278:
3273:
3268:
3263:
3258:
3253:
3248:
3243:
3238:
3233:
3228:
3223:
3222:
3221:
3211:
3206:
3201:
3196:
3191:
3186:
3180:
3178:
3174:
3173:
3171:, 1963–present
3165:
3164:
3157:
3150:
3142:
3133:
3132:
3130:
3129:
3124:
3115:
3112:
3111:
3109:
3108:
3103:
3098:
3093:
3088:
3083:
3078:
3073:
3068:
3063:
3057:
3055:
3051:
3050:
3048:
3047:
3042:
3037:
3032:
3027:
3022:
3017:
3012:
3007:
3002:
2997:
2992:
2987:
2982:
2977:
2972:
2967:
2962:
2957:
2952:
2947:
2942:
2937:
2932:
2927:
2922:
2917:
2912:
2907:
2902:
2897:
2892:
2886:
2884:
2880:
2879:
2876:
2875:
2873:
2872:
2866:
2864:
2860:
2859:
2857:
2856:
2851:
2846:
2841:
2836:
2831:
2826:
2821:
2816:
2811:
2805:
2803:
2796:
2792:
2791:
2782:
2781:
2774:
2767:
2759:
2750:
2749:
2747:
2746:
2741:
2736:
2731:
2726:
2721:
2716:
2711:
2705:
2703:
2697:
2696:
2693:
2692:
2690:
2689:
2684:
2679:
2674:
2669:
2663:
2661:
2657:
2656:
2654:
2653:
2648:
2643:
2638:
2632:
2630:
2623:
2619:
2618:
2615:
2614:
2612:
2611:
2606:
2601:
2596:
2591:
2586:
2581:
2576:
2571:
2566:
2561:
2555:
2553:
2549:
2548:
2545:
2544:
2542:
2541:
2536:
2531:
2526:
2521:
2516:
2511:
2506:
2501:
2496:
2490:
2488:
2484:
2483:
2481:
2480:
2475:
2470:
2465:
2460:
2455:
2450:
2444:
2442:
2433:
2429:
2428:
2426:
2425:
2419:
2417:
2413:
2412:
2410:
2409:
2404:
2399:
2394:
2389:
2384:
2379:
2374:
2368:
2366:
2359:
2355:
2354:
2351:
2350:
2348:
2347:
2342:
2337:
2332:
2327:
2322:
2317:
2312:
2307:
2302:
2297:
2292:
2287:
2282:
2277:
2272:
2267:
2262:
2257:
2252:
2246:
2244:
2240:
2239:
2237:
2236:
2231:
2226:
2221:
2216:
2210:
2208:
2202:
2201:
2199:
2198:
2192:
2190:
2184:
2183:
2181:
2180:
2175:
2169:
2167:
2161:
2160:
2158:
2157:
2152:
2147:
2141:
2139:
2130:
2126:
2125:
2118:
2116:
2113:
2112:
2110:
2109:
2104:
2099:
2093:
2091:
2087:
2086:
2083:
2082:
2080:
2079:
2077:Delta IV Heavy
2074:
2069:
2064:
2058:
2056:
2052:
2051:
2049:
2048:
2043:
2038:
2033:
2028:
2023:
2018:
2013:
2008:
2003:
1997:
1995:
1991:
1990:
1988:
1987:
1982:
1977:
1972:
1967:
1962:
1957:
1952:
1947:
1942:
1937:
1931:
1929:
1922:
1918:
1917:
1915:
1914:
1909:
1904:
1899:
1894:
1889:
1884:
1879:
1874:
1868:
1866:
1859:
1855:
1854:
1852:
1851:
1846:
1841:
1835:
1832:
1831:
1826:
1825:
1818:
1811:
1803:
1797:
1796:
1791:
1786:
1781:
1776:
1771:
1763:
1762:External links
1760:
1758:
1757:
1756:. p. 449.
1738:
1737:. p. 178.
1725:Jefford, C.G.
1721:
1718:
1717:
1716:
1709:
1702:
1683:
1668:
1649:
1634:
1621:
1618:
1617:
1614:
1613:
1599:
1577:
1562:
1547:
1520:
1509:
1476:
1459:
1446:
1420:
1419:
1417:
1414:
1413:
1412:
1411:
1410:
1405:
1400:
1390:
1385:
1380:
1375:
1364:
1363:
1356:
1353:
1352:
1351:
1348:
1345:
1342:
1339:
1336:
1333:
1330:
1327:
1324:
1321:
1318:
1315:
1312:
1309:
1308:
1307:
1301:
1300:(6.02 PJ)
1291:
1285:
1275:
1274:
1273:
1270:
1267:
1264:
1261:
1258:
1255:
1252:
1249:
1246:
1243:
1240:
1230:
1227:
1217:
1214:
1211:
1208:
1205:
1202:
1196:
1190:
1184:
1161:
1158:
1157:
1156:
1155:
1154:
1153:
1152:
1151:
1150:
1148:Leicestershire
1137:
1131:RAF Harrington
1124:
1118:RAF Folkingham
1111:
1098:
1082:
1081:
1080:
1067:
1065:Cambridgeshire
1054:
1041:
1028:
1014:Feltwell Wing
1007:
1006:
1005:
1004:
1003:
990:
977:
964:
951:
935:
934:
933:
920:
907:
894:
881:
867:Hemswell Wing
858:Bomber Command
848:
847:
845:
843:United Kingdom
826:
825:
823:
800:
797:
781:launch vehicle
773:Main article:
770:
769:Launch vehicle
767:
744:
741:
740:
739:
736:Bluegill Prime
732:
725:Starfish Prime
720:
713:
704:
701:
620:Main article:
617:
614:
565:
562:
521:
518:
432:
429:
379:
378:
375:
372:
371:booster engine
361:
358:
348:
335:, formerly of
327:(US Navy) and
301:
298:
257:
254:
197:
196:
193:
189:
188:
185:
180:
177:
176:
173:
169:
168:
164:
163:
160:
156:
155:
152:
148:
147:
144:
140:
139:
138:Specifications
135:
134:
125:
121:
120:
117:
110:
109:
106:
102:
101:
96:
92:
91:
88:
84:
83:
79:
78:
67:
63:
62:
58:
57:
54:
50:
49:
44:
40:
39:
36:
28:
27:
17:
9:
6:
4:
3:
2:
7436:
7425:
7422:
7420:
7417:
7415:
7412:
7410:
7407:
7405:
7402:
7400:
7397:
7395:
7392:
7390:
7387:
7386:
7384:
7374:
7364:
7362:
7352:
7350:
7340:
7339:
7336:
7322:
7316:
7313:
7308:
7306:
7303:
7298:
7293:
7288:
7286:
7283:
7278:
7277:
7275:
7271:
7262:
7260:
7257:
7252:
7250:
7247:
7242:
7240:
7237:
7232:
7230:
7227:
7222:
7217:
7212:
7207:
7202:
7200:
7197:
7192:
7190:
7187:
7185:
7182:
7177:
7172:
7167:
7163:
7160:
7158:
7155:
7154:
7152:
7147:
7142:
7141:
7139:
7135:
7126:
7124:
7121:
7116:
7114:
7111:
7106:
7104:
7101:
7099:
7096:
7094:
7091:
7086:
7081:
7076:
7071:
7069:
7066:
7061:
7060:
7058:
7054:
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2209:
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2171:
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2127:
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2034:
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2024:
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2019:
2017:
2014:
2012:
2009:
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1986:
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1968:
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1910:
1908:
1905:
1903:
1900:
1898:
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1893:
1890:
1888:
1885:
1883:
1882:Thor-Ablestar
1880:
1878:
1875:
1873:
1870:
1869:
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1863:
1860:
1856:
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1847:
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1777:
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1772:
1769:
1766:
1765:
1755:
1754:0-11-772833-0
1751:
1747:
1743:
1739:
1736:
1735:1-85310-053-6
1732:
1728:
1724:
1723:
1714:
1710:
1707:
1703:
1700:
1699:0-8131-2245-7
1696:
1692:
1688:
1684:
1681:
1677:
1673:
1670:Boyes, John.
1669:
1666:
1662:
1658:
1654:
1651:Boyes, John.
1650:
1647:
1643:
1639:
1636:Boyes, John.
1635:
1632:
1628:
1625:Boyes, John.
1624:
1623:
1609:
1603:
1595:
1588:
1581:
1573:
1566:
1558:
1557:Life Magazine
1551:
1543:
1539:
1535:
1531:
1524:
1518:
1513:
1497:
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1371:
1370:
1369:
1368:
1367:Related lists
1362:
1361:Project Emily
1359:
1358:
1349:
1346:
1343:
1340:
1337:
1334:
1331:
1328:
1325:
1322:
1319:
1316:
1313:
1310:
1305:
1302:
1299:
1295:
1292:
1289:
1288:warhead mass:
1286:
1283:
1279:
1278:
1276:
1271:
1268:
1265:
1262:
1259:
1256:
1253:
1250:
1247:
1244:
1241:
1239:
1238:RP-1 Kerosene
1235:
1232:Propellants:
1231:
1228:
1225:
1221:
1220:
1218:
1215:
1212:
1209:
1206:
1203:
1200:
1199:Empty weight:
1197:
1194:
1191:
1188:
1185:
1182:
1179:
1178:
1177:
1175:
1171:
1167:
1149:
1145:
1141:
1138:
1136:
1132:
1128:
1125:
1123:
1119:
1115:
1112:
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1106:
1105:RAF Polebrook
1102:
1099:
1097:
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1085:
1083:
1079:
1075:
1071:
1068:
1066:
1062:
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1049:
1048:RAF Tuddenham
1045:
1042:
1040:
1036:
1032:
1029:
1027:
1023:
1019:
1016:
1015:
1013:
1012:
1011:
1008:
1002:
998:
997:RAF Breighton
994:
991:
989:
985:
981:
978:
976:
972:
968:
965:
963:
959:
955:
952:
950:
946:
945:RAF Driffield
942:
939:
938:
936:
932:
928:
924:
921:
919:
915:
911:
908:
906:
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898:
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844:
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831:
830:
824:
822:
821:United States
811:
810:
805:
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794:
790:
786:
782:
776:
766:
763:
759:
758:Life Magazine
755:
751:
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733:
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721:
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648:
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637:
633:
628:
623:
622:Project Emily
613:
609:
605:
601:
598:
594:
589:
587:
583:
579:
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571:
561:
553:
549:
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468:
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460:
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437:
428:
424:
422:
417:
415:
411:
407:
406:AC Spark Plug
403:
399:
395:
391:
386:
384:
376:
373:
370:
366:
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359:
356:
353:
349:
346:
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326:
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314:
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297:
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282:
280:
276:
272:
271:Project Emily
268:
263:
253:
251:
247:
243:
238:
235:
231:
226:
224:
220:
216:
212:
208:
204:
194:
190:
186:
178:
174:
170:
165:
161:
157:
153:
149:
145:
141:
136:
133:
129:
128:Delta rockets
126:
122:
118:
111:
107:
103:
100:
97:
93:
89:
85:
80:
76:
71:
68:
64:
59:
56:United States
55:
51:
48:
45:
41:
34:
29:
22:
16:
7009:
5072:
4372:
4243:Undesignated
3270:
3118:
3101:Sky Scorcher
2954:
2432:Upper Stages
2416:First stages
2129:Launch sites
1928:Alphabetical
1912:Thorad-Agena
1871:
1849:Delta family
1838:
1741:
1726:
1712:
1705:
1690:
1686:
1671:
1656:
1652:
1637:
1630:
1626:
1602:
1593:
1580:
1571:
1565:
1556:
1550:
1533:
1523:
1512:
1500:. Retrieved
1491:
1479:
1469:
1462:
1454:
1449:
1437:. Retrieved
1433:
1424:
1366:
1365:
1341:Failures: 14
1338:Launches: 59
1303:
1293:
1287:
1222:Vernier: 2x
1198:
1192:
1186:
1180:
1163:
1122:Lincolnshire
1022:RAF Feltwell
931:Lincolnshire
918:Lincolnshire
905:Lincolnshire
892:Lincolnshire
879:Lincolnshire
875:RAF Hemswell
849:
827:
778:
757:
753:
749:
746:
698:
690:
679:
667:
663:RAF Feltwell
653:under US-UK
640:
610:
606:
602:
590:
567:
558:
534:
531:
510:
506:
502:
495:
492:
488:
480:
477:
473:
469:
465:
461:
457:
442:
425:
418:
387:
380:
357:Globemaster)
341:Nazi Germany
318:
283:
275:Jupiter MRBM
262:Soviet Union
259:
239:
227:
221:(IRBM) with
203:PGM-17A Thor
202:
200:
95:Manufacturer
66:Used by
15:
4340:Senior Prom
3378:LGM-35 (II)
3061:Alpha Draco
2883:Other types
2188:Tanegashima
1907:Thor DSV-2U
1892:Thor-Burner
1844:Thor family
1839:PGM-17 Thor
1594:Weatherwise
1326:Flown: 145.
1263:Chambers: 1
1174:Thor DSV-2U
1170:Thor DSV-2J
1010:No. 3 Group
984:RAF Catfoss
971:RAF Carnaby
927:RAF Caistor
901:RAF Bardney
863:No. 1 Group
754:Weatherwise
290:Program 437
181:Operational
116: built
7383:Categories
4057:AGM-158A/B
3373:AQM-35 (I)
3086:Pye Wacket
3076:High Virgo
3066:Bold Orion
2785:1955–1962
2677:Rocketdyne
2358:Components
2300:Harrington
2290:Folkingham
2206:Vandenberg
2046:Delta 9000
2041:Delta 8000
2036:Delta 7000
2031:Delta 6000
2026:Delta 5000
2021:Delta 4000
2016:Delta 3000
2011:Delta 2000
2006:Delta 1000
2001:Delta 0100
1902:Thor DSV-2
1897:Thor-Delta
1887:Thor-Agena
1744:. London:
1416:References
1408:Thor-Delta
1403:Thor-Agena
1166:Thor DSV-2
616:Deployment
597:submarines
402:Rocketdyne
244:and later
172:Propellant
5236:A/B/E/F/N
4373:See also:
4285:Have Dash
3649:AGM-84H/K
3348:MGM-31A/B
3119:See also:
2744:2020–2024
2739:2010–2019
2734:2000–2009
2729:1990–1999
2724:1980–1989
2719:1970–1979
2714:1960–1969
2709:1957–1959
2387:Castor-4A
2345:Tuddenham
2335:Polebrook
2280:Driffield
2255:Breighton
2137:Canaveral
2067:Delta III
1994:Numerical
1877:Thor-Able
1665:1361-4231
1398:Thor-Able
1219:Engines:
1061:RAF Mepal
1001:Yorkshire
988:Yorkshire
975:Yorkshire
962:Yorkshire
949:Yorkshire
483:Thor-Able
471:tankage.
410:Bell Labs
381:Thor had
367:-derived
315:, Florida
309:Thor-Able
108:1959–1960
72:(testing)
7373:Aviation
4148:AIM-174B
4062:AGM-158C
3799:BGM-109G
3696:"AIM-92"
3071:Cherokee
2701:Launches
2499:Ablestar
2382:Castor-4
2377:Castor-1
2372:Castor-1
2365:Boosters
2305:Hemswell
2285:Feltwell
2165:Johnston
2145:(S)LC-17
2072:Delta IV
2062:Delta II
1748:, 1994.
1502:6 August
1496:Archived
1439:16 March
1355:See also
1277:Warhead
793:Delta IV
789:Delta II
717:Starfish
710:Bluegill
686:megatons
655:dual key
572:and the
570:Chrysler
394:Lockheed
159:Diameter
124:Variants
105:Produced
87:Designed
7335:Portals
7310:957–967
7280:900–951
7273:900–999
7264:847–899
7254:835–845
7234:824–831
7194:808–816
7137:800–899
7128:755–799
7118:746–753
7063:700–735
7056:700–799
6440:A/B (I)
6295:600–699
6286:593–599
6266:581–589
6246:571–579
6236:561–569
6216:551–559
6196:543–549
6186:531–541
6176:521–529
6166:501–519
6154:500–599
5277:400–499
5248:381–397
5228:338–379
4978:300–399
4964:280–298
4954:240–278
4944:227–238
4777:200–299
4736:143–197
4435:100–199
4350:Wagtail
4330:OpFires
4250:Aequare
4234:MIM-401
4229:AIM-260
4213:AGM-187
4208:MQM-186
4203:MQM-185
4198:RGM-184
4193:AGM-183
4188:LGM-182
4183:AGM-181
4178:AGM-180
4173:AGM-179
4168:MQM-178
4163:BQM-177
4158:AGM-176
4153:MQM-175
4144:RIM-174
4139:GQM-173
4134:FGM-172
4129:MQM-171
4124:MQM-170
4119:AGM-169
4114:MGM-168
4109:BQM-167
4104:MGM-166
4099:RGM-165
4094:MGM-164
4089:GQM-163
4084:RIM-162
4079:RIM-161
4074:ADM-160
4069:AGM-159
4052:MGM-157
4047:RIM-156
4042:BQM-155
4037:AGM-154
4032:AGM-153
4027:AIM-152
4022:FQM-151
4015:151–200
4006:PQM-150
4001:PQM-149
3996:FGM-148
3991:BQM-147
3986:MIM-146
3981:BQM-145
3976:ADM-144
3971:MQM-143
3966:AGM-142
3961:ADM-141
3956:MGM-140
3951:RUM-139
3946:CEM-138
3941:AGM-137
3936:AGM-136
3931:ASM-135
3926:MGM-134
3921:UGM-133
3916:AIM-132
3911:AGM-131
3906:AGM-130
3901:AGM-129
3896:AQM-128
3891:AQM-127
3886:BQM-126
3876:AGM-124
3871:AGM-123
3866:AGM-122
3856:AIM-120
3851:AGM-119
3846:LGM-118
3841:FQM-117
3836:RIM-116
3831:MIM-115
3826:AGM-114
3821:RIM-113
3816:AGM-112
3811:BQM-111
3806:BGM-110
3789:BQM-108
3784:MQM-107
3779:BQM-106
3774:MQM-105
3769:MIM-104
3764:AQM-103
3759:PQM-102
3754:RIM-101
3747:101–150
3738:LIM-100
3644:AGM-84E
3448:XLIM-49
3352:MGM-31C
3316:LGM-25C
3311:HGM-25A
3096:Skydart
2870:AIM-101
2682:Thiokol
2672:Alliant
2667:Aerojet
2660:Engines
2636:Douglas
2552:Engines
2473:Delta-P
2468:Delta-K
2463:Delta-F
2458:Delta-E
2453:Delta-D
2448:Delta-A
2270:Catfoss
2265:Carnaby
2260:Caistor
2250:Bardney
2155:SLC-37B
1985:Delta N
1980:Delta M
1975:Delta L
1970:Delta J
1965:Delta G
1960:Delta F
1955:Delta E
1950:Delta D
1945:Delta C
1940:Delta B
1935:Delta A
1858:Rockets
1655:. pub:
1193:Weight:
1096:Rutland
1078:Norfolk
1052:Suffolk
1039:Suffolk
1026:Norfolk
593:US Navy
390:Douglas
352:Douglas
311:at the
256:History
230:Jupiter
209:of the
7162:L (II)
7025:S (II)
6755:A (II)
6690:A (II)
6445:B (II)
6068:L (II)
5852:L (II)
5590:G (II)
5448:M (II)
4345:Sprint
3733:LIM-99
3728:YQM-98
3723:AIM-97
3718:UGM-96
3713:AIM-95
3708:YQM-94
3703:XQM-93
3691:FIM-92
3686:AQM-91
3681:BQM-90
3676:UGM-89
3671:AGM-88
3666:AGM-87
3661:AGM-86
3656:RIM-85
3634:AGM-83
3629:AIM-82
3624:AQM-81
3619:AGM-80
3614:AGM-79
3609:AGM-78
3604:FGM-77
3599:AGM-76
3594:BGM-75
3589:BQM-74
3584:UGM-73
3579:MIM-72
3574:BGM-71
3569:LEM-70
3564:AGM-69
3559:AIM-68
3554:RIM-67
3549:RIM-66
3544:AGM-65
3539:AGM-64
3534:AGM-63
3529:AGM-62
3524:MQM-61
3519:AQM-60
3514:RGM-59
3509:MQM-58
3504:MQM-57
3499:PQM-56
3494:RIM-55
3489:AIM-54
3484:AGM-53
3479:MGM-52
3474:MGM-51
3467:51–100
3458:RIM-50
3453:LIM-49
3443:AGM-48
3438:AIM-47
3433:MIM-46
3428:AGM-45
3423:UUM-44
3418:FIM-43
3413:MQM-42
3408:AQM-41
3403:MQM-40
3398:MQM-39
3393:AQM-38
3388:AQM-37
3383:MQM-36
3368:AQM-34
3363:MQM-33
3358:MGM-32
3343:LGM-30
3338:MGM-29
3333:AGM-28
3328:UGM-27
3323:AIM-26
3306:RIM-24
3301:MIM-23
3296:AGM-22
3291:MGM-21
3286:ADM-20
3281:PGM-19
3276:MGM-18
3271:PGM-17
3266:CGM-16
3261:RGM-15
3256:MIM-14
3246:AGM-12
3241:PGM-11
3236:CIM-10
3091:Skokie
3081:Jaguar
3020:SRM-88
3015:GAM-87
2995:GAM-83
2975:GAM-79
2965:GAM-77
2940:GAM-72
2935:GAM-71
2915:GAM-67
2900:GAM-63
2854:GAR-11
2646:Boeing
2629:Rocket
2609:TR-201
2574:B-8096
2569:B-8081
2564:B-8048
2539:UM-129
2514:Burner
2509:Altair
2407:GEM-60
2402:GEM-46
2397:GEM-40
2234:SLC-10
2150:LC-18B
2090:Export
2055:Modern
1752:
1733:
1697:
1678:
1663:
1644:
1608:"Thor"
1294:Yield:
840:
818:
671:apogee
396:, and
365:Navaho
151:Length
7157:L (I)
7020:S (I)
6750:A (I)
6685:A (I)
6088:L (I)
6063:L (I)
5847:L (I)
5585:G (I)
5443:M (I)
5289:B/C/N
4360:GLSDB
4320:NCADE
4310:MA-31
4260:Brazo
4255:ASALM
3231:AIM-9
3226:RIM-8
3219:RIM-7
3214:AIM-7
3209:RGM-6
3204:MGM-5
3199:AIM-4
3194:MIM-3
3189:RIM-2
3184:MGM-1
3045:IM-99
3040:RM-92
3035:RM-91
3030:RM-90
3025:RM-89
3010:RM-86
3005:RM-85
3000:RM-84
2990:RM-82
2985:RM-81
2980:SM-80
2970:SM-78
2960:TM-76
2955:SM-75
2950:SM-74
2945:SM-73
2930:IM-70
2925:IM-69
2920:SM-68
2910:SM-65
2905:SM-64
2895:SM-62
2890:TM-61
2849:GAR-9
2844:GAR-8
2839:GAR-6
2834:GAR-5
2829:GAR-4
2824:GAR-3
2819:GAR-2
2814:GAR-1
2604:RS-68
2599:RS-27
2584:LR-79
2529:PAM-D
2519:FW-4D
2504:Agena
2487:Other
2440:Delta
2320:Mepal
2243:Bases
2229:SLC-6
2224:SLC-3
2219:SLC-2
2214:SLC-1
2196:Osaki
1921:Delta
1590:(PDF)
1187:Span:
785:Delta
693:Atlas
634:) in
453:Atlas
445:LC-17
369:Atlas
355:C-124
279:ICBMs
246:Delta
234:Atlas
183:range
7153:802
6976:695
6941:691
6911:687
6876:683
6856:681
6801:672
6761:666
6746:665
6681:655
6611:649
6591:648
6511:634
6436:621
6336:603
6321:602
6306:601
6250:580
6220:560
6200:550
6129:499
6099:498
6079:497
6059:495
6024:490
5989:485
5969:484
5905:478
5868:474
5843:471
5726:451
5686:445
5651:441
5611:435
5581:431
5556:428
5541:427
5526:426
5469:418
5434:416
5414:414
5330:405
5257:399
5232:380
5069:315
5014:306
4908:222
4788:201
4670:132
4558:118
4543:117
4483:107
4335:PrSM
4325:NLOS
4315:MSDM
4305:LRHW
4300:LREW
4280:HACM
4275:HALO
4222:201–
3177:1–50
2809:MB-1
2594:RL10
2589:R-4D
2579:LE-5
2559:AJ10
2534:Star
2524:IABS
2494:Able
2478:DCSS
2178:LE-2
2173:LE-1
2102:N-II
1872:Thor
1865:Thor
1768:Thor
1750:ISBN
1746:HMSO
1731:ISBN
1695:ISBN
1676:ISBN
1661:ISSN
1642:ISBN
1504:2013
1441:2020
1304:CEP:
1280:One
555:rear
421:MA-3
242:Thor
201:The
143:Mass
90:1957
43:Type
7315:968
7305:956
7300:855
7295:854
7290:853
7285:952
7259:846
7249:834
7244:833
7239:832
7229:823
7224:822
7219:821
7214:820
7209:819
7204:818
7199:817
7189:807
7184:806
7179:805
7174:804
7169:803
7149:801
7144:800
7123:754
7113:745
7108:744
7103:743
7098:742
7093:741
7088:740
7083:739
7078:738
7073:737
7068:736
7047:699
7042:698
7037:697
7032:696
6972:694
6967:693
6962:692
6937:690
6932:689
6927:688
6907:686
6902:685
6897:684
6872:682
6852:680
6847:679
6842:678
6837:677
6832:676
6827:675
6822:674
6817:673
6810:M/P
6797:671
6792:670
6787:669
6782:668
6777:667
6770:C/P
6742:664
6737:663
6732:662
6727:661
6722:660
6717:659
6712:658
6707:657
6702:656
6677:654
6672:653
6667:652
6662:651
6657:650
6587:647
6582:646
6577:645
6572:644
6567:643
6562:642
6557:641
6552:640
6547:639
6542:638
6537:637
6532:636
6527:635
6507:633
6502:632
6497:631
6492:630
6487:629
6482:628
6477:627
6472:626
6467:625
6462:624
6457:623
6452:622
6432:620
6427:619
6422:618
6417:617
6412:616
6407:615
6402:614
6397:613
6392:612
6387:611
6382:610
6377:609
6372:608
6367:607
6362:606
6357:605
6352:604
6302:600
6281:592
6276:591
6271:590
6241:570
6191:542
6181:530
6171:520
6161:500
6075:496
6055:494
6050:493
6045:492
6040:491
6020:489
6015:488
6010:487
6005:486
5965:483
5958:M/Z
5943:482
5931:481
5926:480
5921:479
5901:477
5889:476
5884:475
5864:473
5859:472
5839:470
5834:469
5829:468
5824:467
5819:466
5814:465
5809:464
5804:463
5799:462
5794:461
5782:460
5777:459
5772:458
5767:457
5762:456
5757:455
5752:454
5747:453
5742:452
5722:450
5717:449
5712:448
5707:447
5702:446
5682:444
5677:443
5672:442
5647:440
5642:439
5637:438
5632:437
5627:436
5607:434
5602:433
5597:432
5577:430
5572:429
5522:425
5517:424
5512:423
5507:422
5502:421
5495:L/W
5490:420
5485:419
5465:417
5430:415
5410:413
5405:412
5388:411
5371:410
5366:409
5361:408
5356:407
5351:406
5326:404
5321:403
5316:402
5311:401
5299:G/H
5284:400
5253:398
5223:337
5218:336
5213:335
5208:334
5203:333
5198:332
5193:331
5188:330
5176:329
5164:328
5152:327
5147:326
5142:325
5135:M/N
5125:324
5120:323
5115:322
5110:321
5105:320
5100:319
5095:318
5090:317
5085:316
5078:A-2
5073:A-1
5065:314
5060:313
5055:312
5050:311
5045:310
5040:309
5035:308
5030:307
5018:A/L
5010:305
5005:304
5000:303
4995:302
4990:301
4985:300
4969:299
4959:279
4949:239
4939:226
4934:225
4929:224
4924:223
4904:221
4899:220
4894:219
4889:218
4884:217
4879:216
4874:215
4869:214
4864:213
4859:212
4854:211
4849:210
4844:209
4839:208
4834:207
4829:206
4824:205
4819:204
4814:203
4809:202
4797:B/W
4792:A/L
4784:200
4746:199
4741:198
4731:142
4726:141
4721:140
4716:139
4711:138
4706:137
4701:136
4696:135
4691:134
4686:133
4666:131
4661:130
4656:129
4651:128
4646:127
4641:126
4636:125
4631:124
4626:123
4621:122
4616:121
4611:120
4584:C/F
4579:119
4539:116
4534:115
4529:114
4524:113
4519:112
4514:111
4509:110
4504:109
4499:108
4492:A-2
4487:A-1
4479:106
4474:105
4469:104
4464:103
4459:102
4447:101
4442:100
4295:KEI
4290:JSM
4270:GBI
2687:TRW
2392:CBC
2107:H-I
2097:N-I
1538:doi
1298:TNT
1282:W49
1234:LOX
661:at
576:in
447:at
321:CEP
114:No.
7385::
1629:.
1592:.
1532:.
1494:.
1490:.
1432:.
1146:,
1142:–
1133:,
1129:–
1120:,
1116:–
1107:,
1103:–
1094:,
1090:–
1076:,
1072:–
1063:,
1059:–
1050:,
1046:–
1037:,
1033:–
1024:,
1020:–
999:,
995:–
986:,
982:–
973:,
969:–
960:,
956:–
947:,
943:–
929:,
925:–
916:,
912:–
903:,
899:–
890:,
886:–
877:,
873:–
688:.
643:UK
516:.
392:,
7337::
7015:R
7010:Q
7005:P
7000:N
6995:L
6990:C
6985:B
6980:A
6955:Z
6950:X
6945:C
6920:P
6915:J
6890:V
6885:J
6880:A
6865:E
6860:D
6805:A
6765:A
6695:P
6650:P
6645:L
6640:F
6635:E
6630:D
6625:C
6620:B
6615:A
6605:P
6600:D
6595:A
6520:B
6515:A
6345:L
6340:A
6330:L
6325:A
6315:L
6310:A
6259:E
6254:A
6229:F
6224:A
6209:E
6204:A
6143:D
6138:C
6133:A
6123:L
6118:E
6113:D
6108:C
6103:A
6093:L
6083:A
6033:M
6028:L
5998:Z
5993:L
5983:N
5978:M
5973:L
5953:L
5948:E
5936:L
5914:T
5909:A
5894:E
5877:N
5872:L
5787:L
5735:L
5730:D
5695:M
5690:L
5665:L
5660:D
5655:A
5620:L
5615:A
5565:L
5560:A
5550:M
5545:L
5535:M
5530:L
5478:M
5473:L
5458:Q
5453:P
5438:L
5423:M
5418:L
5398:L
5393:E
5381:L
5376:E
5346:D
5341:C
5334:B
5304:M
5294:E
5266:B
5261:A
5241:P
5181:F
5169:E
5157:E
5130:L
5023:B
4917:G
4912:A
4802:E
4766:Y
4761:D
4756:C
4751:B
4679:B
4674:A
4604:Y
4599:T
4594:L
4589:E
4572:P
4567:L
4562:A
4552:M
4547:L
4452:P
4419:e
4412:t
4405:v
4146:/
3354:)
3350:(
3161:e
3154:t
3147:v
2778:e
2771:t
2764:v
1822:e
1815:t
1808:v
1701:.
1682:.
1667:.
1648:.
1610:.
1544:.
1540::
1506:.
1443:.
1236:/
731:.
331:(
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