66-402: B53 or B-53 may refer to : B53 nuclear bomb HLA-B53 , an HLA-B serotype Convair XB-53 , an American aircraft [REDACTED] Topics referred to by the same term This disambiguation page lists articles associated with the same title formed as a letter–number combination. If an internal link led you here, you may wish to change
132-457: A 20-mile (32 km) radius (1,250 sq mi or 3,200 km ). Blast effects would be sufficient to collapse most residential and industrial structures within a 9 mi (14 km) radius (254 sq mi or 660 km ); within 3.65 mi (5.87 km) (42 sq mi or 110 km ) virtually all above-ground structures would be destroyed and blast effects would inflict near 100% fatalities. Within 2.25 mi (3.62 km)
198-668: A 3300 volt 2.0 μF capacitor for the firing set. If neither the radar fuze or the contact crystals actuated, the weapon would detonate at 120 seconds from arming. The weapons were to initially use the MC4175 Trajectory Sensing Signal Generators which are identical to the TSSG found in the B61-7, but starting from 1991, the Mod 6 was to get a new MC4137 Trajectory Sensing Signal Generator. The MC4175 stored
264-526: A 500- rem (5- sievert ) dose of ionizing radiation would be received by the average person, sufficient to cause a 50% to 90% casualty rate independent of thermal or blast effects at this distance. Currently, seven actual B53s are on display at the following facilities or museums. B61 nuclear bomb The B61 nuclear bomb is the primary thermonuclear gravity bomb in the United States Enduring Stockpile following
330-471: A ground burst to create a crater and destroy it through the shockwave. A 50-kiloton yield detonating on the ground produces a crater with a radius of 30–68 meters, depending on the density of the surface, effectively putting the bunker within the circular error probability . In 2014 critics said that a more accurate and less destructive nuclear weapon would make leaders less cautious about deploying it, while Schwartz said it would deter adversaries more because
396-614: A non-fissile ( lead or tungsten ) secondary casing. The explosive yield for the Y1 version was declassified in 2014 as being 9 Mt. In 1988, some B53s were upgraded to the B53 Mod 1 (B53-1) variant to improve weapon safety and to provide compatibility with the G/H variants of the B52 bomber. During this upgrade the weapon lost full-fuzing capability, retaining only the laydown fuzing mode. The B53-1 had
462-411: A parachute retarder (currently a 24-ft (7.3 m) diameter nylon / Kevlar chute). This offers the aircraft a chance to escape the blast in its retarded delivery modes, or allows the weapon to survive impact with the ground in laydown delivery mode. Contact preclusion can also be selected by the pilot. The weapon can be released at speeds up to Mach 2 and altitudes as low as 50 feet (15 m). In one of
528-564: A second successful test in August 2017. Despite claims the Mod 12 has an earth penetrating capability, the weapon does not have the reinforced structure like that of the Mod 11, which is required to function as an earth penetrating weapon. The Mod 11 will be retained in service for the ground penetrating mission. The Mod 12 Life Extension Program continued in 2018 and on 29 June 2018 two successful non-nuclear system qualification flight tests at Tonopah Test Range were reported. In October 2018,
594-559: A selectable laydown time of 30 to 240 seconds in 30 second increments. It was intended as a bunker buster weapon, using a surface blast after laydown deployment to transmit a shock wave through the earth to collapse its target. Attacks against the Soviet deep underground leadership shelters in the Chekhov / Sharapovo area south of Moscow envisaged multiple B53/W53 exploding at ground level. It has since been supplanted in such roles by
660-478: A spin of 5 revolutions per second. This was to improve stability and decoupling during high speed delivery. Three alternatives to the weapon were also explored for still-classified reasons. The first alternative was halted due to its similarity to the original TX-61 design, and the Department of Defense was unfavorable to the second option which halted its exploration. The TX-61 design was ordered to "proceed along
726-457: A streamlined casing capable of withstanding supersonic flight and is 11 ft 8 in (3.56 m) long, with a diameter of about 13 inches (33 cm). The basic weight of the B-61 is about 700 pounds (320 kg), although the weights of individual weapons may vary depending on version and fuze /retardation configuration. As of 2020, the weapon was undergoing a 12th modification. According to
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#1732773253244792-402: A streamlined casing capable of withstanding supersonic flight. The original B61-0 weapon was 141.6 inches (3.60 m) long, with a diameter of 13.3 inches (340 mm) and a basic weight of 715 pounds (324 kg) with most later weapons having approximately the same dimensions and weight, except for the Mod 11 version which has a weight of approximately 1,200 pounds (540 kg). The B61
858-459: A target; the Mod 11 nuclear earth-penetrator is accurate to 110–170 meters from the desired detonation location, so it requires a 400-kiloton warhead. The Mod 12 is accurate to 30 meters from a target and only requires a 50-kiloton warhead. Schwartz believes that greater accuracy would both improve the weapon and create a different target set it can be useful against. An example is the higher-yield Mod 11's role of attacking underground bunkers that need
924-622: A variety of US military aircraft. US aircraft cleared for its use have included the B-1 Lancer , B-2 Spirit , B-52 Stratofortress , F/A-18 Hornet , A-6 Intruder , A-4 Skyhawk , F-111 , F-15E Strike Eagle and F-16 Fighting Falcon and the F-35A . As part of NATO Nuclear Weapons Sharing, German and Italian Panavia Tornado aircraft can also carry B61s. The B61 can fit inside the F-22 Raptor 's weapons bays and will also be carried by
990-485: A yield of 8.9 Megatons . The Mk 53 entered production in 1962 and was built through June 1965. About 340 bombs were built. It entered service aboard B-47 Stratojet , B-52G Stratofortress , and B-58 Hustler bomber aircraft in the mid-1960s. From 1968 it was redesignated B53 . Some early versions of the bomb were dismantled beginning in 1967. After the Titan II program ended, the remaining W-53s were retired in
1056-587: Is armed by ground-based personnel via an access panel located on the side of the bomb, which opens to reveal nine dials, two sockets, and a T-handle which manually triggers the "command disable" function. One of the sockets is for a MC4142 "strike enable" plug which must be inserted in order to complete critical circuits in the safety/arming and firing mechanisms. The other socket is the PAL connector, which has 23 pins marked with alphabetic letter codes. The B61 "command disable" mechanism functions as follows: after entering
1122-476: Is identical to the battery used on the B61-7 and is thermally operated, providing 120 seconds of power for the weapon, but initial power is supplied by the MC2238 Pulse Batteries which are activated by the weapon's pullout switches during separation from the aircraft. The weapon contained two neutron generators for initiation, used a 2400 volt 0.6 μF capacitor for neutron generator firing and
1188-668: The B-21 Raider , but it is not planned to be deployed on the F-35. The Federation of American Scientists have accused the weapon of being a "political bomb", introduced to finally retire the B83-1 nuclear bomb, whose retirement has been blocked by hardliners. A W61 Earth Penetrator Warhead (EPW) with a yield of 340 kilotonnes of TNT (1,400 TJ) was developed for the AGM-129 Advanced Cruise Missile and
1254-680: The B57 nuclear bomb . Environmental conditions specified included an indefinite temperature range of −60 °F (−51 °C) to 160 °F (71 °C), shocks of up to 40g, and in flight temperatures of up to 275 °F (135 °C) for up to 40 minutes. Parachute deployment was specified to produce a maximum load of 255 g (2,500 m/s ). The weapon was designed and built by the Los Alamos National Laboratory in New Mexico . Production engineering began in 1965, with
1320-496: The Federation of American Scientists in 2012, the roughly 400 B61-12s will each cost "more than its weight in gold" - $ 28 million apiece. In 1961 a report was issued indicating Navy and Air Force interest in a lightweight bomb to replace existing weapons, but that both services had considerably different military requirements for such a weapon. However, the authors of the report believed that due to advances in technology it
1386-940: The Lockheed Martin F-35 Lightning II . B61 tactical variants are deployed with NATO allies in Europe as part of the NATO Nuclear Weapons Sharing Program . About 150 bombs are stored at six bases: Kleine Brogel in Belgium, Büchel Air Base in Germany, Aviano and Ghedi Air Base in Italy, Volkel Air Base in the Netherlands and Incirlik in Turkey. In 2012, NATO agreed to improve the capabilities of this force with
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#17327732532441452-865: The MGM-134 Midgetman small ICBM. The weapon entered Phase 1 initial development in January 1985 and phase 4 production engineering in September 1992 before being cancelled in December of that year. In the Advanced Cruise Missile role, the weapon was to replace aging B53 bombs, but after the W61 cancellation the role was filled by the B61-11 bomb. A declassified technical report on the automation of pit handling at Pantex indicates that
1518-603: The Titan II ICBM used the same physics package as the B53, without the air drop-specific components like the parachute system and crushable structures in the nose and sides needed for lay-down delivery, reducing its mass to about 6,200 lb (2,800 kg). The 8,140-pound (3,690 kg) Mark-6 re-entry vehicle containing the W53 warhead was about 123 inches (10.3 ft; 3.1 m) long, 7.5 feet (2.3 m) in diameter and
1584-639: The "hedge" portion of the Enduring Stockpile until its complete dismantling in 2011. The last B53 was disassembled on 25 October 2011, a year ahead of schedule. With its retirement, the largest bomb currently in service in the U.S. nuclear arsenal is the B83 , with a maximum yield of 1.2 megatons. The B53 was replaced in the bunker-busting role by the B61 Mod 11 . Development of the weapon began in 1955 by Los Alamos National Laboratory , based on
1650-502: The 2012 Production and Planning Directive are being retained in an indeterminate state pending a senior-level government evaluation of their use in planetary defense against earthbound asteroids ." In its FY2015 budget request, the NNSA noted that the B53 component disassembly was "delayed", leading some observers to conclude they might be the warhead CSAs being retained for potential planetary defense purposes. The W-53 nuclear warhead of
1716-487: The 400 weapons is now expected to cost over $ 10 billion. The Mod 12 tail assembly contract was awarded to Boeing on November 27, 2012 for $ 178 million. Boeing will use their experience with the Joint Direct Attack Munition to yield JDAM-equivalent accuracy in a nuclear bomb. This contract is only the first part of the billion-dollar expense of producing and applying the tail kits, over and above
1782-795: The B61 is hoped to lead to the retirement of the B83, resulting in the elimination of the last megaton-yield U.S. bomb and leave the B61-series as the only U.S. gravity nuclear bomb. In 2013, the Pentagon and NNSA stated that if B61 refurbishment did not begin by 2019, components in the existing weapons could begin to fail. In 2013 Tom Collina of the Arms Control Association said that the new development could complicate arms control efforts with Russia. In 2014, Congress slashed funding for
1848-690: The B61-2 and B61-5 share a common pit design, as do the B61-3, B61-10 and W85. The B61-0 and B61-4 do not share a pit with any other weapon. As the B61-7 was a retrofit of the B61-1 and the B61-11 was a retrofit of the B61-7, they presumably share a common pit. In May 2010 the National Nuclear Security Administration asked Congress for $ 40 million to redesign the bomb to enable the Lockheed Martin F-35 Lightning II to carry
1914-943: The B61-5 contained beryllium and that if the use of beryllium were to be restricted, the B61-5 could probably be replaced by the B61 Mod 3. The B61 Mod 6 and Mod 8 bombs were developed for use by the US Navy beginning in March 1987 and cancelled at the end of the Cold War. The weapons weighed 350 kilograms (770 lb), had a length of 3,597 millimetres (141.6 in) and a diameter of 338 millimetres (13.3 in), and were one-point safe, used insensitive high explosives (IHE) in their primary stages and utilized enhanced electrical safety (EES). The weapons were to be built by converting existing B61-0, −2 and −5 weapons into Mod 6 and 8 weapons and
1980-549: The Kosvinsky completion date is regarded as one explanation for U.S. interest in a new nuclear bunker buster and the declaration of the deployment of the Mod 11 in 1997: Kosvinsky is protected by about 1,000 feet (300 m) of granite . The B61 unguided bomb should not be confused with the MGM-1 Matador cruise missile , which was originally developed under the bomber designation B-61. The B61 has been deployed by
2046-591: The MC2935 come from either of the two MC4175s or the MC4137 Trajectory Sensing Signal Generators. A third stronglink existed inside the first exclusion region of the weapon and was involved in weapon arming. Details of the system are still classified. As of 2013 the Pentagon saw the B83 nuclear bomb as a "relic of the Cold War," believing that deploying a megaton-yield gravity bomb, the highest level nuclear weapon left in
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2112-559: The MC2969 in the open position until a specific unlock signal was received. The second stronglink was the MC2935 Trajectory Stronglink Switch of which there were two, one for each channel of the weapon's firing set. Like the MC2969, it mechanically locked if it received the wrong input signals, but unlike the MC2969 it could only be manually unlocked, which could only take place at the factory. Signals for
2178-513: The MC4139 and continuously applied power the MC4137 does not know how to arm the safelink. The weapon was to feature a number of weapon stronglinks. Stronglinks are part of the weapon's safety systems and are designed to be robust enough that they can survive abnormal environments long enough for the weapon's weaklinks to fail. This requires weak and stronglinks to be colocated so they are exposed to
2244-585: The Mod 12 guided tail-kit assembly received Milestone C approval to enter the production phase; the TKA went through the traditional test program in under 11 months, achieving a 100% success rate for all 31 bomb drops. The B61-12 nuclear bomb completed its successful flight tests with the US Air Force's F-15E in June 2020. It was dropped from above 25,000ft and was in the air for approximately 55 seconds before hitting
2310-631: The Russian Deputy Minister of Foreign Affairs Alexander Grushko , who accused the US government of "reducing the nuclear threshold" with the weapon's increased accuracy. The F/A-18E/F Super Hornet is not listed as a future platform. Initially, the NNSA Stockpile Stewardship and Management Plan anticipated Phase 1 development for the B61 Mod 13 Life Extension Program (LEP) beginning in 2037 with first production of
2376-552: The U.S. inventory, to Europe was "inconceivable" at this point. It can also only be carried by the B-2 bomber, and integrating it onto additional aircraft would be costly. The Mod 12 upgrade is being pursued as a forward-deployed tactical/strategic nuclear weapon to protect NATO and Asian allies since it can be used from dual-capable fighter aircraft, as well as planned to arm the F-35 and B-21 Raider , and its lower yield options make it more flexible with less collateral effects. Recapitalizing
2442-420: The U.S. would be more willing to use it in situations where necessary. The improved accuracy would make it more effective than the previous Mod 3/4 currently deployed to the continent. F-16 and Panavia Tornado aircraft cannot interface with the new bomb due to electronic differences, but NATO countries buying the F-35 would be able to utilize it. The first flight test for an inert Mod 12 was conducted in 2015, with
2508-569: The W53 warhead some distance away. Due to the safety measures built into the weapon, it did not explode or release any radioactive material . Fifty-two active missiles were deployed in silos prior to the beginning of the retirement program in October 1982. Assuming a detonation at optimum height, a 9-megaton blast would result in a fireball with an approximate 2.9 to 3.4 mi (4.7 to 5.5 km) diameter. The radiated heat would be sufficient to cause lethal burns to any unprotected person within
2574-445: The W53 warhead, the 800-to-900 lb (360-to-410 kg) parachute system and the honeycomb aluminum nose cone to enable the bomb to survive laydown delivery . It had five parachutes: one 5-foot (1.52 m) pilot chute , one 16-foot (4.88 m) extractor chute, and three 48-foot (14.63 m) main chutes. Chute deployment depends on delivery mode, with the main chutes used only for laydown delivery. For free-fall delivery,
2640-561: The arming signal for the trajectory stronglink in its memory, so it featured a pair of rolamite acceleration switches designed to prevent the possibility of the signal being transferred to the stronglink before the rolamites were actuated by the spinning of the weapon in flight. The MC4137 instead is provided the unique signal from the MC4139 Programmer, which stores it in a volatile memory that erases after approximately seven seconds of lost power, meaning that without intent from
2706-418: The bomb incapable of being used. Any B61 which has had the command disable facility activated must be returned to Pantex for repair. The B61 can be set for airburst or groundburst detonation, and by free fall , retarded free fall or laydown delivery through the use of a parachute to slow down the weapon during release from the delivery aircraft. Only the Mod 0 to 10 versions of the B61 are equipped with
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2772-451: The correct three-digit numeric code it is then possible to turn a dial to "DI" and pull back a T-shaped handle which comes away in the user's hand. This action releases a spring-loaded firing pin which fires the percussion cap on an MC4246A thermal battery , powering it up. Electrical power from the thermal battery is sufficient to "fry" the internal circuitry of the bomb, destroying critical mechanisms without causing detonation. This makes
2838-599: The earlier Mk 21 and Mk 46 weapons. In March 1958 the Strategic Air Command issued a request for a new Class C (less than five tons, megaton-range) bomb to replace the earlier Mk 41 . A revised version of the Mk 46 became the TX-53 in 1959. The development TX-53 warhead was apparently never tested, although an experimental TX-46 predecessor design was detonated 28 June 1958 as Hardtack Oak, which detonated at
2904-425: The earth-penetrating B61 Mod 11 , a bomb that penetrates the surface to deliver much more of its explosive energy into the ground, and therefore needs a much smaller yield to produce the same effects. The B53 was intended to be retired in the 1980s, but 50 units remained in the active stockpile until the deployment of the B61-11 in 1997. At that point the obsolete B53s were slated for immediate disassembly; however,
2970-597: The end of the Cold War . It is a low-to-intermediate yield strategic and tactical nuclear weapon featuring a two-stage radiation implosion design. The B61 is of the variable yield ("dial-a-yield" in informal military jargon) design with a yield of 0.3 to 340 kilotons in its various mods ("modifications"). It is a Full Fuzing Option (FUFO) weapon, meaning it is equipped with the full range of fuzing and delivery options, including air and ground burst fuzing, and free-fall, retarded free-fall and laydown delivery. It has
3036-517: The entire system was jettisoned. The W53 warhead of the B53 used oralloy (highly enriched uranium ) instead of plutonium for fission, with a mix of lithium -6 deuteride fuel for fusion. The explosive lens comprised a mixture of RDX and TNT , which was not insensitive . Two variants were made: the B53-Y1 , a "dirty" weapon using a U-238-encased secondary, and the B53-Y2 "clean" version with
3102-575: The first war-reserve B61-0 weapon accepted by the AEC in December 1966. However production was halted in May 1967 for design modifications to be made before resuming in January 1968. Shot Flintlock Halfbeak in June 1966 may have been a full yield test of the weapon with other tests conducted between 1963 and 1968 at the Nevada Test Site. During testing, spin motors were added to the weapon to produce
3168-681: The increased accuracy of the Mod 12 upgrade and the delivery of the F-35 aircraft. This added a modest standoff capability to the B61. The F-35A was certified to carry the B61-12 in October 2023, marking the first time a fifth generation fighter has been nuclear capable, and the first new platform in the NATO inventory to achieve such status since the early 1990s. The B61 is a variable yield ("dial-a-yield" colloquially) dual use tactical and strategic bomb equipped with Full Fuzing Option (FUFO) designed for external carriage by high-speed aircraft. It has
3234-526: The late 1980s. The B53 was retired in 1986, but in 1988 50 units were brought back into service and received the B53 Mod 1 safety upgrade so the air force could cover certain targets previously covered by Titan II. These weapons remained in the active stockpile until the deployment of the B61-11 in 1997. At that point the obsolete B53s were slated for immediate disassembly; however, the process of disassembling
3300-402: The lines" of the third alternative in May 1964, though it is unclear what that means. Total production of all versions was approximately 3,155, of which approximately 540 remain in active service, 415 in inactive service and 520 are awaiting dismantlement as of 2012 . 13 versions of the B61 have been designed, known as Mod 0 through Mod 12. Of these, nine have entered production. Each shares
3366-399: The link to point directly to the intended article. Retrieved from " https://en.wikipedia.org/w/index.php?title=B53&oldid=932703984 " Category : Letter–number combination disambiguation pages Hidden categories: Short description is different from Wikidata All article disambiguation pages All disambiguation pages B53 nuclear bomb The Mk/B53
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#17327732532443432-563: The primary carrier for the Mod 11 is the B-2 Spirit . As of 2023, the B61 has 13 variants, referred to as Mod 0 through Mod 12. A Sandia document on the dates of the development phases of the US nuclear stockpile describes the B61-3 as an "improved Mod 2 w/IHE" and the B61-4 as "same as Mod 3 ex. Hi-Y". The B61 Mod 3 and 4 bombs do not contain beryllium . A 1978 report on reducing or substituting beryllium in nuclear weapons noted that
3498-604: The process of disassembling the units was greatly hampered by safety concerns as well as a lack of resources. The last remaining B53 bomb began the disassembly processes on Tuesday, 25 October 2011 at the Energy Department's Pantex Plant . An April 2014 GAO report notes that the National Nuclear Security Administration (NNSA) is retaining canned sub-assemblies (CSAs) "associated with a certain warhead indicated as excess in
3564-542: The program was that the new weapon would modernize the nuclear arsenal, improve the capability of aircraft and simplify the nuclear weapons inventory by replacing lower-yield versions of the B28 and B43 nuclear bombs . The desired production date was June 1965. The weapon was designated the TX-61 in January 1963. Due to the short time-scales, it was decided to make maximum use of off-the-shelf components such as those developed for
3630-409: The project and called for alternates to be studied. In January 2014, former Air Force Chief of Staff Norton A. Schwartz stated that the Mod 12 nuclear bomb upgrade would have enhanced accuracy and a lower yield with less fallout compared to previous versions of the weapon. Accuracy has not been a guarantee for air-dropped nuclear weapons, so consequently large warheads were needed to effectively impact
3696-401: The same physics package , with different yield options. The newest variant is the Mod 11, deployed in 1997, which is a ground-penetrating bunker busting weapon. The Russian Continuity of Government facility at Kosvinsky Kamen , finished in early 1996, was designed to resist US earth-penetrating warheads and serves a similar role as the American Cheyenne Mountain Complex . The timing of
3762-401: The same environmental conditions in an accident. The first stronglink was the MC2969 Intent Stronglink Switch which was also used on the B61-3, −4 and −7, W78, W80 and B83 weapons. The MC2969 consisted of a 14-pin ceramic-insulated bank of switches that would close upon the receipt of the proper intent unique signal (IUQS) to its electromechanical decoder. Receipt of the wrong signal would lock
3828-401: The target. The first B61-12 bomb was produced in November 2021. The weapon replaces the B61 mod 3, mod 4 and mod 7 bombs while the B61-11 will be retained in the stockpile. It is expected that the LEP will extend the B61's life by at least 20 years. Politico reported in October 2022 that the US military planned to accelerate the deployment of the Mod 12 in Europe. This drew criticism from
3894-441: The units was greatly hampered by safety concerns as well as a lack of resources. In 2010 authorization was given to disassemble the 50 bombs at the Pantex plant in Texas. The process of dismantling the last remaining B53 bomb in the stockpile was completed in 2011. The B53 was 12 feet 4 inches (3.76 m) long with a diameter of 50 inches (4.17 ft; 1.27 m). It weighed 8,850 pounds (4,010 kg), including
3960-502: The weapon in 2050, but in 2023 plans were announced to produce a new gravity bomb similar to that of the B61-12, but having a high yield similar to that of the B61-7, named the B61 Mod 13. This discards plans for the Mod 13 to be a future Mod 12 LEP. It is planned that for each B61-13 produced, one fewer B61-12 is to be produced, therefore not increasing the planned number of new B61 bombs; defense officials indicated only "a few dozen" B61-13s may be produced. The new bomb will be carried by
4026-402: The weapon internally by 2017. This version is designated Mod 12. The four hundred Mod 12 bombs will be used by both tactical aircraft (such as the F-35) and strategic aircraft (such as the B-2) and the Tail Subassembly (TSA) will give them Joint Direct Attack Munition levels of accuracy, allowing the fifty kiloton warhead to have strategic effects from all carrying aircraft. However, refitting
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#17327732532444092-513: The weapon's laydown modes, it detonates 31 seconds after weapon release. The Mod 11 is a hardened penetration bomb with a reinforced casing and a delayed-action fuze ; this allows the weapon to penetrate several metres into the ground before detonating, damaging fortified structures further underground. Developed from 1994, the Mod 11 went into service in 1997 replacing the older megaton -yield B53 bomb . About 50 Mod 11 bombs have been produced, their warheads converted from Mod 7 bombs. At present,
4158-404: The weapons were to use B61-7 weapon parts where possible. By mass, the largest deviations from the B61-7 were the Acorn assembly, MC4137 TSSG (trajectory sensing signal generator) and the JTA (described as "ballast for WR"). The weapon's computer was the MC4139 Programmer, two of which are used on independent channels, and is identical to the programmer used on the B61-7. The MC3656 Main Battery
4224-538: Was a high-yield bunker buster thermonuclear weapon developed by the United States during the Cold War . Deployed on Strategic Air Command bombers, the B53, with a yield of 9 megatons, was the most powerful weapon in the U.S. nuclear arsenal after the last B41 nuclear bombs were retired in 1976. The B53 was the basis of the W-53 warhead carried by the Titan II missile , which was decommissioned in 1987. Although not in active service for many years before 2010, fifty B53s were retained during that time as part of
4290-444: Was mounted atop a spacer which was 8.3 feet (2.5 m) in diameter at the missile interface (compared to the missile's core diameter of 10 feet [3.0 m]). With a yield of 9 megatons , it was the highest yield warhead ever deployed on a US missile. About 65 W53 warheads were constructed between December 1962 and December 1963. On 19 September 1980 a fuel leak caused a Titan II to explode within its silo in Arkansas , throwing
4356-401: Was possible for a single weapon to fulfill both requirements. This was followed by a report from Sandia in mid-1962, that believed that a lightweight nuclear bomb with full fuzing option was possible and that such a program could be completed in a short time-span, possibly by 1965 or 1966. Development of the weapon that would become the B61 was authorized in December 1962. The justification for
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