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B36 In Neopangaia
In UMMO/Neopangaia, the world is a post apocalyptic one. During the ensuing wars fought with genetically engineered soldiers and other monstrosities, dropped from massive remanufactured Peacemaker Bombers).
Each bomber is equipped with a variety of futuristic propulsion, cloaking, phasing, and teleportation devices upon request. in addition, they are popular flying “fortresses” for Sky Pirates.
Some of them have even been retrofitted for “satellite hunting” or inter-dimensional bombardment. They are the only flight capable combat chassis large enough to handle air dropping Mecha into the battlefield.
During the wars, thousands of Peacemaker chassis, in a variety of materials, can be found all over the globe. Their precious cargo of information, Mecha, and corresponding genetic material is highly sought after.
Nyarlathotep uses this design as the basis for the Nation’s newest combat bomber.
Convair B-36 (wiki)
|The B-36D used both piston and jet engines.|
|Designed by||Ted Hall|
|First flight||8 August 1946|
|Retired||12 February 1959|
|Primary user||United States Air Force|
|Unit cost||US$4.1 million (B-36D)|
The Convair B-36 (nicknamed Peacemaker) was a strategic bomber built by Convair and operated solely by the United States Air Force (USAF). The B-36 was the largest mass-produced piston engined aircraft ever made and had the largest wingspan in a combat aircraft ever built (230 ft (70 m)), although there have been larger military transports. The B-36 was the first bomber capable of delivering thermonuclear weapons from within a fully-enclosed bomb-bay. With a range of over 6,000 miles (9,700 km) and a maximum payload of at least 72,000 lb (33,000 kg), the B-36 was the first operational bomber with an intercontinental range, setting the standard for subsequent USAF long range bombers, such as the B-52 Stratofortress, B-1 Lancer, and B-2 Spirit.
The genesis of the B-36 can be traced to early 1941, prior to the entry of the U.S. into World War II. At that time it appeared that there was a very real chance that Britain could fall, making a strategic bombing effort by the U.S. against Germany impossible. A new class of bomber would be needed to fill this role, one offering trans-Atlantic range so it could bomb targets in Europe from bases inside the continental USA. The United States Army Air Corps opened up a design competition for the very long-range bomber on 11 April 1941, asking for a 450 mph (720 km/h) top speed, a 275 mph (443 km/h) cruising speed, a service ceiling of 45,000 ft (14,000 m), and a maximum range of 12,000 miles (19,000 km) at 25,000 ft. These proved too demanding for any short-term design, so on 19 August 1941 they were reduced to a maximum range of 10,000 miles (16,000 km), an effective combat radius of 4,000 miles (6,400 km) with a 10,000 pound bombload, a cruising speed between 240 and 300 mph (480 km/h), and a service ceiling of 40,000 ft.
After the Cold War began in earnest with the 1948 Berlin Airlift and the 1949 atmospheric test of the first Soviet atomic bomb, American military planners sought bombers capable of delivering the very large and heavy first-generation nuclear bombs. The B-36 was the only American aircraft with the range and payload to carry such bombs from airfields on American soil to targets in the USSR (storing nuclear weapons in foreign countries was, and remains, diplomatically sensitive).
The B-36 was arguably obsolete from the outset, being piston-powered in a world of jet interceptors, but its jet rival, the B-47 Stratojet, which did not become fully operational until 1953, lacked the range to attack the Soviet homeland from North America and could not carry the huge first-generation hydrogen bomb. Nor could the other American piston bombers of the day, the B-29 or B-50. Intercontinental ballistic missiles (ICBMs) did not become effective deterrents until the 1960s. Until the B-52 Stratofortress became operational in the late 1950s, the B-36, as the only truly intercontinental bomber, was the mainstay of the Strategic Air Command (SAC).
Convair touted the B-36 as an “aluminum overcast”, a “long rifle” to give SAC a global reach. When General Curtis LeMay headed SAC (1949–57) and turned it into an effective nuclear delivery force, the B-36 formed the heart of his command. Its maximum payload was more than four times that of the B-29, even exceeding that of the B-52. The B-36 was slow and could not refuel in the air, but could fly missions to targets 3,400 miles (5,500 km) away and stay aloft as long as 40 hours.Moreover, the B-36 was believed to have an ace up its sleeve: a high cruising altitude, made possible by its huge wing area, that put it out of reach of all piston fighters and early jet interceptors.
Nevertheless, the B-36 was difficult to operate, prone in its early service years to catastrophic engine fires and other costly malfunctions. To its critics, these problems made it a “billion-dollar blunder”. In particular, the United States Navy saw it as a costly bungle diverting Congressional funding and interest from naval aviation and aircraft carriers in general, and carrier–based nuclear bombers in particular. In 1947, the Navy attacked Congressional funding for the B-36, alleging it failed to meet Pentagon requirements. The Navy believed the dominance of the aircraft carrier in the Pacific during World War II proved carrier-based air strikes would be decisive in future wars. To this end, the Navy designed the USS United States (CVA-58), a “supercarrier” capable of launching huge fleets of tactical aircraft or nuclear bombers. It then pushed to have funding transferred from the B-36 to the USS United States. The Air Force successfully defended the B-36 project, and the United States was officially cancelled by Secretary of Defense Louis A. Johnson in a cost-cutting move. Several high-level Navy officials questioned the government’s decision, alleging a conflict of interest because Johnson had once served on Convair’s Board of Directors. The uproar following the cancellation of United States was nicknamed the “Revolt of the Admirals“.
The furor, as well as the significant use of aircraft carriers in the Korean War, resulted in the design and procurement of the subsequent Forrestal class of supercarriers, which were of comparable size to the United States but with a design geared towards greater multirole use with composite air wings of fighter, attack, reconnaissance, electronic warfare, early warning and antisubmarine warfare aircraft. At the same time, heavy manned bombers for the Strategic Air Command were also deemed crucial to national defense and, as a result, the two systems were never again in competition for the same budgetary resources.
Design and development
In 1941, the fall of Britain to a German invasion seemed imminent. This would have left the United States Army Air Corps (AAC) with no bases in Europe from which to bomb Germany. American bombers would have had to reach Europe from bases in North America, necessitating a combat range of at least 5,700 miles (9,200 km), the length of a Gander, Newfoundland–Berlin round trip. The AAC therefore sought a bomber of truly intercontinental range.
On 11 April 1941, the USAAC announced a design competition for an aircraft with a 275 mph (445 km/h) cruising speed, a service ceiling of 45,000 ft (14,000 m), capable of delivering 10,000 lb (4,500 kg) of bombs to targets 10,000 miles (16,000 km) away. These requirements far exceeded the technology of the day. The B-36 concept began with a proposal by Consolidated Vultee Aircraft Corporation (later Convair) to meet this requirement; the same design request led to the Northrop YB-35. Though the need to bomb Germany from North American bases never arose, the project was not cancelled because the B-36 was seen as playing a possible eventual role in the Pacific war.
The B-36 took shape as an aircraft of immense proportions, two-thirds longer than the previous “superbomber”, the B-29. The wingspan and tail height of the B-36 exceeded those of the Antonov An-22, the largest ever mass-produced propeller-driven aircraft. Only with the advent of the Boeing 747 and the Lockheed C-5 Galaxy, both designed two decades later, did aircraft capable of lifting a heavier payload than the B-36 become routine.
The wings of the B-36 were large even when compared with present-day aircraft, exceeding, for example, those of the C-5 Galaxy, and enabled the B-36 to carry enough fuel to fly very long missions without refueling. The wing area permitted cruising altitudes above the operating ceiling of 1940s-era fighters, jet as well as piston. All versions of the B-36 could cruise at over 40,000 ft (12,000 m). B-36 mission logs commonly recorded mock attacks against U.S. cities while flying at 49,000. In 1954, the turrets and other nonessential equipment were removed, resulting in a “featherweight” configuration believed to have resulted in a top speed of 423 mph (700 km/h), and cruise at 50,000 ft (15,000 m) and dash at over 55,000ft (16,800M), perhaps even higher.
The large wing area and the option of starting the jet engines gave the B-36 a wide margin between stall speed (VS) and maximum speed (Vmax) at these altitudes. This made the B-36 more maneuverable at high altitude than the USAF jet interceptors of the day, which either could not fly above 40,000 ft (12,000 m), or if they did, were likely to stall out when trying to maneuver or fire their guns. However, the Navy argued that their F2H Banshee fighter could intercept the B-36, thanks to its ability to operate at more than 50,000 ft. The Air Force declined the Navy’s invitation to a fly-off between the Banshee and the B-36. Later, the new Secretary of Defense, Louis A. Johnson, whose personal biases was such that he considered the U.S. Navy and Naval Aviation essentially obsolete in favor of the U.S. Air Force and Strategic Air Command, forbade putting the Navy’s claim to the test.
The propulsion system alone made the B-36 a very unusual aircraft. All B-36s featured six Pratt & Whitney R-4360 Wasp Major radial piston engines. Even though the prototype R-4360s delivered a total of 18,000 hp (13.4 MW), early B-36s were slow and required long takeoff runs. The situation improved with later versions delivering 3,800 hp (2.8 MW) apiece. Each engine drove an immense three-bladed propeller, 19 ft (5.8 m) in diameter, mounted in the pusher configuration. This unusual configuration prevented propeller turbulence from interfering with airflow over the wing.
Beginning with the B-36D, Convair suspended a pair of General Electric J47-19 jet engines from each wing; these were also retrofitted to all extant B-36Bs. Thus the B-36 came to have 10 engines, more than any other mass-produced aircraft. The jet pods greatly improved takeoff performance and dash speed over the target. In normal cruising flight, the jet engines were shut down to conserve fuel.
The B-36 had a crew of 15. As in the B-29, the pressurized flight deck and crew compartment were linked to the rear compartment by a pressurized tunnel through the bomb bay. In the B-36, one rode through the tunnel on a wheeled trolley, by pulling oneself on a rope. The rear compartment led to the rear turret, and featured six bunks and a galley. The B-36 also tested the experimental Boston Camera.
The XB-36 featured single-wheel landing gear whose tires were the largest ever manufactured up to that time, 9 ft, 2 in (2.7 m) tall, 3 ft (1 m) wide, and weighing 1,320 lb (600 kg), with enough rubber for 60 automobile tires. These tires placed so much weight per unit area on runways, the XB-36 was restricted to the Fort Worth airfield next to where it was manufactured, and to a mere two USAF bases. At the suggestion of General Henry H. Arnold, the single-wheel gear was soon replaced by a more conventional four-wheel bogie. At one point a tank-like tracked landing gear was also tried on the XB-36, but proved heavy and noisy and was quickly abandoned.
The four bomb bays could carry up to 86,000 pounds of bombs, more than 10 times the load carried by the World War II workhorse, the B-17 Flying Fortress, and substantially more than the B-17’s gross weight. The B-36 was not designed with nuclear weaponry in mind, because the mere existence of such weapons was top secret during most of the period when the B-36 was engineered (1941–46), and their mode of delivery had yet to be determined. Nevertheless, the B-36 stepped into a nuclear delivery role immediately upon becoming operational. In all respects but speed, the B-36 could match what was arguably its approximate Soviet counterpart, the Tu-95, which began production in January 1956 and is still in service. Until the B-52 came on line, the B-36 was the only means of delivering the first generation Mark-17 hydrogen bomb, 25 ft (7.5 m) long, 5 ft (1.5 m) in diameter, and weighing 42,000 lb (19,000 kg), the heaviest and bulkiest American nuclear weapon ever. Carrying this massive weapon required merging two adjacent bomb bays.
The defensive armament consisted of six remote-controlled retractable gun turrets, and fixed tail and nose turrets. Each turret was fitted with two 20 mm cannon, for a total of 16 cannons, the greatest defensive firepower ever carried by a bomber. Recoil from gunnery practice could cause the vacuum-tube electronics to malfunction, solid state then being unknown. This contributed to the crash of B-36B 44-92035 on 22 November 1950.
The first prototype XB-36 flew on 8 August 1946. The speed and range of the prototype failed to meet the standards set out by the Army Air Corps in 1941. As is often the case with aircraft pushing the size envelope, the XB-36 experienced a number of problems. (For instance, the B-29 Superfortress was plagued by engine problems, and available engines were too weak to afford the Boeing XB-15 a useful top speed.)
A second aircraft, the YB-36, flew on 4 December 1947. It featured a redesigned high-visibility “bubble” canopy, which was later adopted for production. Altogether, the YB-36 was much closer to the production aircraft. Additionally, the engines used on the YB-36 were a good deal more powerful and more efficient.
The first of 21 B-36As were delivered in 1948. They were admitted interim airframes, intended for crew training and later conversion. No defensive armament was fitted as none was ready. Once later models were available, all B-36As were converted to RB-36E reconnaissance models. The first B-36 variant meant for normal operation was the B-36B, delivered beginning in November 1948. This aircraft met all the 1941 requirements, but had serious problems with engine reliability, and with the availability of armaments and spare parts. Later models featured more powerful variants of the R-4360 engine, improved radar, and redesigned crew compartments.
The four jet engines raised fuel consumption, thus reducing range. Meanwhile, new air-to-air missiles made hand-aimed guns mounted in heavy turrets obsolete; they were also unreliable. In February 1954, the USAF awarded Convair a contract to reduce the weight of the entire B-36 fleet by implementing a new “Featherweight” design program in three configurations:
- Featherweight I removed the 6 movable gun turrets and other defensive hardware.
- Featherweight II removed the rear compartment crew comfort features, and all hardware accommodating the XF-85 parasite fighter.
- Featherweight III incorporated both configurations I and II.
The six turrets eliminated by Featherweight I reduced the aircraft’s crew from 15 to 9. Featherweight III enabled a longer range and an operating ceiling of at least 47,000 ft (14,000 m), features especially valuable for reconnaissance missions. The B-36J-III configuration (the last 14 made) featured a single radar-aimed tail turret, extra fuel tanks in the outer wings, and landing gear allowing the maximum gross weight to rise to 410,000 pounds (190,000 kg). Production of the B-36 ceased in 1954.
- Prototype powered by six 3,000 hp (2,200 kW) R-4360-25 engines and unarmed, one built.
- Prototype with modified nose and raised cockpit roof, one built later converted to YB-36A.
- Former YB-36 with modified four-wheel landing gear, later modified as a RB-36E.
- Production variant, unarmed used for training, 22 built all but one converted to RB-36E.
- Armed production variant with six 3,500 hp (2,600 kW) R-4360-41 engines, 73 built later conversions to RB-36D and B-36D.
- Designation for 39 B-36Bs temporary fitted with a camera installation.
- Projected variant of the B-36B with six 4,300 hp (3,200 kW) R-4360-51 engines driving tractor propellers, not built.
- Production version of the YB-36 completed as B-36Bs.
- Same as B-36B but fitted with four J47-GE-19 engines, two each in two underwing pods, 22 built and 64 conversions from B-36B.
- Strategic reconnaissance variant with two bomb bays fitted with camera installation, 17 built and seven conversions from B-36B.
- The YB-36A and 21 B-36As converted to RB-36D standards.
- Same as B-36D but fitted with six 3,800 hp (2,800 kW) R-4360-53 engines and four J47-GE-19 engines, 34 built.
- Strategic reconnaissance variant of the B-36F with additional fuels capacity, 24 built.
- One RB-36F modified to carry a GRF-84F Thunderstreak on a ventral trapeze as part of the FICON program.
- Project for a jet-powered swept wing variant due to the difference between a standard B-36 it was re-designated the YB-60.
- Same as B-36F with improved cockpit and equipment changes, 83 built.
- One B-36H fitted with a nuclear reactor installation for trials, had a revised cockpit and raised nose.
- Strategic reconnaissance variant of the B-36H, 73 built.
- High altitude variant with strengthened landing gear, increased fuel capacity, armament reduced to tail guns only and reduced crew, 33 built.
More than a third of all B-36 models were reconnaissance models, designated RB-36. Before the development of the Lockheed U-2, the RB-36 was the mainstay of American photo reconnaissance over hostile territory. It was the only American aircraft having range enough to fly into Asia from bases in the USA, and size enough to carry the bulky high-resolution cameras of the day. The RB-36 performed a number of rarely acknowledged reconnaissance missions and is suspected of having carried out numerous penetrations of Chinese (and possibly Soviet) airspace.
The RB-36 was well-suited for such reconnaissance missions. Its high cruising altitude made it difficult to intercept, and its fuel capacity enabled missions up to 50 hours long. The RB-36 featured a pressurized camera compartment staffed by a crew of seven, in place of a forward bomb bay. The aft bomb bay contained tanks for extra fuel. The RB-36 cameras could produce very high resolution photographs: pictures of a golf course taken from 40,000 ft (12,000 m) show recognizable golf balls. RB-36s were distinguished by the bright aluminium of the camera compartment (contrasting with the dull magnesium of the rest of the fuselage) and by a series of radar domes under the aft fuselage, varying in number and placement.
The B-36, including its RGB-36, RB-36, and XC-99 variants, was in service as part of the USAF Strategic Air Command from 1948 through 1958. Its principal operating units and locations were the 5th Bombardment Wing and 9th Strategic Reconnaissance Wing at Fairfield-Suisun AFB, later renamed Travis AFB, California; 6th Bombardment Wing at Walker AFB, New Mexico, 7th Bombardment Wing and 11th Bombardment Wing at Carswell AFB, Texas; 28th Bombardment Wing at Ellsworth AFB, South Dakota; 42nd Bombardment Wing at Loring AFB, Maine; 72nd Bombardment Wing at Ramey AFB, Puerto Rico; 92nd Bombardment Wing and 99th Bombardment Wing at Fairchild AFB, Washington; and the 95th Bombardment Wing at Biggs AFB, Texas.
The B-36 was too large to fit in most hangars. Moreover, even an aircraft with the range of the B-36 needed to be stationed as close to the enemy as possible, and this meant the northern continental United States, Alaska, and the Arctic. As a result, most “normal” maintenance, such as changing the 56 spark plugs (always at risk of fouling by the leaded fuel of the day) on each of its six engines, or replacing the dozens of bomb bay light bulbs shattered after a gunnery mission, was performed outdoors, in 100 °F (38 °C) summers or −60 °F (−51.1 °C) winters, depending on the location. Special shelters were built so that the maintenance crews could enjoy a modicum of protection while working on the engines. Often, ground crews were at risk of slipping and falling from icy wings, or being blown off the wings by a propeller running in reverse pitch.
The wing roots were thick enough, 7 ft (2.1 m), to enable a flight engineer to access the engines and landing gear by crawling through the wings. This was possible only at altitudes not requiring pressurization.
The Wasp Major engines also had a prodigious appetite for lubricating oil, each engine requiring its own 100 gallon (380 L) tank. A former ground crewman has written: “[I don’t recall] an oil change interval as I think the oil consumption factor handled that.” It was not unusual for a mission to end simply because one or more engines ran out of oil.
Like all large aircraft powered by piston engines, the B-36 was prone to engine fires. The problem was exacerbated by the pusher configuration, which facilitated carburetor icing. The design of the R-4360 engine tacitly assumed that it would be mounted in the conventional tractor configuration – propeller/air intake/28 cylinders/carburetor – with air flowing in that order. In this configuration, the carburetor is bathed in air warmed by engine cooling and so is unlikely to ice up. However, the R-4360 engines in the B-36 were mounted in the pusher configuration – air intake/carburetor/28 cylinders/propeller. The carburetor was now in front of the engine and so could not benefit from engine heat, and also made more traditional short term carb heat systems unsuitable. Hence when intake air was cold and humid, ice gradually obstructed the carburetor air intake, which in turn gradually increased the richness of the air/fuel mixture until the unburned fuel in the exhaust caught fire. Three engine fires of this nature led to the first loss of an American nuclear weapon, described below (an event known as a broken arrow in military terminology).
Training missions were typically in two parts; first, a 40 hour flight – followed by some time on the ground for refueling and maintenance – then a 24 hour second flight. With a sufficiently light load, the B-36 could fly at least 10,000 miles (16,000 km) nonstop, and the highest cruising speed of any version, the B-36J-III, was only 230 mph (380 km/h). Turning the jet engines on could raise the cruising speed to over 400 mph (650 km/h), but the resulting higher fuel consumption reduced the range. Hence a 40-hour mission, with the jets used only for takeoff and climbing, flew about 9,200 miles (15,000 km).
The B-36 was not a particularly enjoyable aircraft to fly. Its overall performance, in terms of speed and manuverability, was never considered sprightly. Lieutenant General James Edmundson likened it to “…sitting on your front porch and flying your house around.” Despite its immense exterior size, the pressurized crew compartments were relatively cramped, especially when occupied for 24 hours by a crew of 15 in full flight kit.
War missions would have been essentially one-way, taking off from forward bases in Alaska or Greenland, overflying the USSR, and landing in Europe or the Middle East. Ironically, recollections of crew veterans reveal that while crews were confident of their ability to complete a mission if called upon to do so, they were less confident of surviving the weapon delivery itself. Their concerns were a function of the relatively low speed of the aircraft coupled with the extreme destructive power of the bombs they were carrying, resulting in the plane still being in harm’s way once the bombs detonated on target. These concerns were borne out by the 1954 Operation Castle tests, in which B-36s flew near detonations in the 15-megaton range, at distances believed typical of wartime delivery, and experienced blast damage.
The B-36 was employed in a variety of aeronautical experiments throughout its service life. Its immense size, range and payload capacity lent itself to use in research and development programs. These included nuclear propulsion studies, and “parasite” programs in which the B-36 carried smaller interceptors or reconnaissance aircraft.
In May 1946, the Air Force began the Nuclear Energy for the Propulsion of Aircraft (NEPA) project which was followed in May 1951 by the Aircraft Nuclear Propulsion (ANP) program. The ANP program required that Convair modify two B-36s under the MX-1589 project. One of the modified B-36s studied shielding requirements for an airborne reactor to determine whether a nuclear aircraft was feasible. The Nuclear Test Aircraft (NTA) was a B-36H-20-CF (Serial Number 51-5712) that had been damaged in a tornado at Carswell AFB on 1 September 1952. This plane, designated the NB-36H, was modified to carry a 1 MW, air-cooled nuclear reactor in the aft bomb bay, with a four ton lead shield between the reactor and the cockpit. The cockpit was encased in lead and rubber, with a 6-inch (15 cm)–thick acrylic glass windshield. The reactor was operational but did not power the plane; its sole purpose was to investigate the effect of radiation on aircraft systems. Between 1955 and 1957, the NB-36H completed 47 test flights and 215 hours of flight time, during 89 of which the reactor was critical.
Other experiments involved providing the B-36 with its own fighter defense in the form of parasite aircraft carried partially or wholly in a bomb bay. One parasite aircraft was the tiny McDonnell XF-85 Goblin, which docked using a trapeze system. The concept was tested successfully using a B-29 carrier, but docking proved difficult even for experienced test pilots. Moreover, the XF-85 was seen as no match for Soviet aircraft, and the project was cancelled.
More successful was the FICON project, involving a modified B-36 – called a GRB-36D “mothership” – and the RF-84K, a fighter modified for reconnaissance, in a bomb bay. The GRB-36D would ferry the RF-84K to the vicinity of the objective, whereupon the RF-84K would disconnect and begin its mission. Ten GRB-36Ds and 25 RF-84ks were built and saw active service until 1959.
Projects TIP TOW and Tom-Tom involved docking F-84s to the wingtips of B-29s and B-36s. The hope was that the increased aspect ratio of the combined aircraft would result in a greater range. Project TIP TOW was canceled when the combination of two EF-84Ds and a specially modified test EB-29A crashed, killing everyone on all three aircraft. This accident was attributed to one of the EF-84Ds flipping over onto the wing of the EB-29A. Project Tom-Tom, involving RF-84Fs and a GRB-36D from the FICON project (redesignated JRB-36F), continued for a few months after this crash, but was also canceled due to the violent turbulence induced by the wingtip vortices of the B-36.
The operational life of the B-36 ended because:
- Long range jet-powered bombers became feasible, resulting in such aircraft as the B-47 and B-52, with cruising speeds more than double that of the B-36.
- The speed and operating ceiling of jet fighter interceptors steadily rose.
- Radar-guided surface-to air missiles, such as the Soviet SA-2 Guideline, capable of reaching 20,000 meters (65,616 ft), emerged.
- The airframe, especially the wings, proved vulnerable to metal fatigue.
- Wing flexing led to fuel leakage, a common problem.
The B-36 was progressively removed from service as the B-52 became operational in 1955. The last B-36s left active USAF service in 1959.
Only four (and a half) B-36 type aircraft survive today, from the 384 produced.
- YB-36/RB-36E AF Serial No. 42-13571. This was the first prototype to be converted to the bubble canopy used on production B-36s. It was on display in the 1950s at the former site of the Air Force Museum, now the National Museum of the United States Air Force, at Wright-Patterson Air Force Base near Dayton, Ohio. When the museum moved to its current location at Wright-Patterson, the cost of moving the bomber was more than simply flying a different B-36 to the new location and the aircraft was slated to be scrapped. Instead, private collector Walter Soplata bought it and transported the pieces by truck to his farm in Newbury, Ohio, where it sits today in several large pieces. The bomb bay currently contains a complete P-47N still packed in its original shipping crate.
- RB-36H AF Serial No. 51-13730, is on display at the Castle Air Museum at the former Castle Air Force Base in Atwater, California.
- B-36J AF Serial No. 52-2217, is on display at the Strategic Air and Space Museum, (formerly located at Offutt Air Force Base) and now just off base near Ashland, Nebraska.
- B-36J AF Serial No. 52-2220, is on display at the National Museum of the United States Air Force (formerly The U.S. Air Force Museum) at Wright-Patterson Air Force Base near Dayton, Ohio. Its flight to the museum from Davis-Monthan Air Force Base in Arizona on 30 April 1959 was the last flight of a B-36. This B-36J replaced the former Air Force Museum’s original YB-36 AF Serial Number 42-13571 (see above). This was also the first aircraft to be placed in the Museum’s new display hangar, and was not moved again until relocated to the Museum’s latest addition in 2003. It is displayed alongside the only surviving example of the massive 9 ft (2.7 m) XB-36 wheel and tire.
- B-36J, AF Serial No. 52-2827, the final B-36 built, named “The City of Fort Worth”, was loaned to the city of Fort Worth, Texas on 12 February 1959. It sat on the field at the Greater Southwest International Airport until that property was redeveloped as a business park. It then moved to the short-lived Southwest Aero Museum, which was located between the former Carswell Air Force Base (now NAS Fort Worth) and the former General Dynamics (now Lockheed Martin) assembly plant. From there it went to the Lockheed Martin plant, where some restoration took place. As Lockheed Martin had no place to display the finished plane, and local community efforts in Fort Worth to build a facility to house and maintain the massive aircraft fell short, the USAF Museum retook possession of the plane and it was transported to Tucson, Arizona for loan to the Pima Air & Space Museum. It is now undergoing restoration and reassembly at the Pima Air & Space Museum, just south of Davis-Monthan AFB, Arizona and will ultimately be displayed at that location.
- XC-99, AF Serial No. 43-52436, the sole example of the cargo version of the B-36, was stored for years at the former Kelly AFB, now the Kelly Field Annex of Lackland AFB, in San Antonio, Texas. It has since been relocated and is currently undergoing restoration and reassembly at the National Museum of the United States Air Force at Wright-Patterson AFB in Dayton, Ohio.
Notable incidents and accidents
Though the B-36 had a better than average overall safety record, 10 B-36s crashed between 1949 and 1954 (three B-36Bs, three B-36Ds, and four B-36Hs). Goleta Air and Space Museum maintains a web site with photographs and lengthy excerpts from the official crash reports. When a crash occurred, the magnesium-rich airframe burned readily.
B-36s were also involved in two “Broken Arrow” incidents. On 13 February 1950, a B-36, serial number 44-92075, crashed in an unpopulated region of British Columbia, resulting in the first loss of an American nuclear weapon (see 1950 British Columbia B-36 crash). It was never confirmed whether the crew ditched the nuclear payload into the north Pacific. Locating the crash site took some effort, and what the USAF recovery team found there was classified.
On 22 May 1957, a B-36 accidentally dropped a Mark-17 hydrogen bomb on a deserted area while landing at Kirtland AFB in Albuquerque, New Mexico. Only the conventional trigger detonated, the bomb being unarmed. These incidents were classified for decades. See list of military nuclear accidents.
In 1951, the USAF asked Convair to build a prototype of an all-jet variant of the B-36. Convair complied by replacing the wings on a B-36F with swept wings, from which were suspended eight Pratt & Whitney XJ57-P-3 jet engines. The result was the B-36G, later renamed the Convair YB-60. The YB-60 was deemed inferior to Boeing’s YB-52, and the project was terminated.
Just as the C-97 was the transport variant of the B-50, the B-36 was the basis for the Convair XC-99, a double-decked military cargo plane that was the largest piston engined, land-based aircraft ever built, and the longest practical aircraft (185 ft, 56 m) of its era. The sole example ever built was extensively employed for nearly a decade, especially for cross-country cargo flights during the Korean War. In 2005, this XC-99 was dismantled in anticipation of its being moved from the former Kelly Air Force Base, now the Kely Field Annex of Lackland AFB in San Antonio, Texas, where it had been retired since 1957. The XC-99 was relocated to the National Museum of the United States Air Force at Wright-Patterson Air Force Base near Dayton, Ohio, with C-5 Galaxy transports carrying pieces of the XC-99 to Wright-Patterson as space and schedule permitted.
In 1949, the B-36 was featured in the documentary film, Target: Peace, which was centered around the operations of the 7th Bombardment Wing at Carswell AFB. Other scenes included B-36 production at the Fort Worth plant.
The B-36 featured prominently in Paramount’s Strategic Air Command (1955), starring James Stewart and June Allyson. In the film Jimmy Stewart’s character is forced to crash land his B-36 in the Arctic. Strategic Air Command features many good aerial shots of B-36s and B-47s and was primarily filmed at Carswell AFB, TX and MacDill AFB, FL.
Throughout its time in service, the B-36 was the subject of USAF lore, some apocryphal, some containing a grain of truth.
- If all engines functioned normally at full power during the pre-takeoff warm up, the lead flight engineer would say to the aircraft commander “six [engines] turning and four [engines] burning”. Inconsistent engine reliability led to the wisecrack “two turning, two burning, two joking and two smoking”, with two engines not accounted for.
Data from
- Crew: 9
- Length: 162 ft 1 in (49.40 m)
- Wingspan: 230 ft 0 in (70.10 m)
- Height: 46 ft 9 in (14.25 m)
- Wing area: 4,772 ft² (443.3 m²)
- Airfoil: NACA 63(420)-422 root, NACA 63(420)-517 tip
- Empty weight: 171,035 lb (77,580 kg)
- Loaded weight: 266,100 lb (120,700 kg)
- Max takeoff weight: 410,000 lb (190,000 kg)
- Maximum speed: 420 mph (365 knots, 685 km/h) with jets on
- Cruise speed: 230 mph (200 knots, 380 km/h) with jets off
- Range: 5,905 nm (10,945 km) with 10,000 lb (4,535 kg) payload
- Ferry range: 10,000 mi (8,700 nm, 16,000 km)
- Service ceiling: 48,000 ft (15,000 m)
- Rate of climb: 1,920 ft/min (9.75 m/s)
- Wing loading: 55.76 lb/ft² (272.3 kg/m²)
- Power/mass (prop): 0.086 hp/lb (120 W/kg)
- Thrust/weight (jet): 0.078
- Guns: 2× 20 mm (0.787 in) M24A1 cannon
- Bombs: 86,000 lb (39,010 kg) with weight restrictions, 72,000 lb (32,660 kg) normal
|Wikimedia Commons has media related to: B-36 Peacemaker|
- B-36 Peacemaker Museum
- B-36B 44-92075
- Convair B-36 variants
- FICON project
- Lycoming R-7755
- Revolt of the Admirals
- Strategic Air Command
- XF-85 Goblin
- “Victory Bomber”
- ^ Knaack, Marcelle Size. Post-World War II Bombers, 1945-1973. Washington, DC: Office of Air Force History, 1988. ISBN 0-16-002260-6.
- ^ Convair proposed the name “Peacemaker” in a submission to a contest to name the bomber. Although the name “Peacemaker” was not officially adopted, it was commonly used and sources often state or imply the name is “official”. Peacemaker Name Certificate, 7th Bomb Wing B-36 Association
- ^ a b c d e f g National Museum of the USAF
- ^ a b Taylor 1969, p. 465.
- ^ Winchester 2006, p. 49.
- ^ Wagner 1968, p. 142.
- ^ Yenne 2004, pp. 124–126.
- ^ original image from the Maxwell Air Force Base website.
- ^ Wolk 2003, p. 163.
- ^ Barlow, Jeffrey G. Revolt of the Admirals: The Fight for Naval Aviation, 1945–1950. Washington, DC: Naval Historical Center, 1994. ISBN 0-16-042094-6.
- ^ a b Johnson 1978, p. 1.
- ^ Jacobsen and Wagner 1980, p. 4.
- ^ compares the large aircraft designed in the 1940s
- ^ Jacobsen 1974, p. 54.
- ^ Yenne 2004, pp. 136–137.
- ^ Jacobson and Meyer, The Big Stick.
- ^ AU/ACSC/166/1998-04 Standard Aircraft Characteristics, F2H-2 Banshee
- ^ Air Command and Staff College Air University, “The Revolt of the Admirals”
- ^ Yenne 2004, pp. 137–138.
- ^ Shiel 1996, p. 7.
- ^ Convair XB-36 Peacemaker Retrieved: 4 September 2006.
- ^ At one point a tank-like tracked landing gear
- ^ Convair XB-36 Landing Gear. National Museum of the United States Air Force.  Retrieved: 4 September 2006.
- ^ Boeing B-17 Product History page
- ^ BBC NEWS | Europe | Russia sparks Cold War scramble
- ^ Mark 17
- ^ Summary of Air Force accident report
- ^ detail on the features and performance of each of 16 variants of the B-36
- ^ “The Last B-36 and the people who saved it from destruction.” 1 October 2006, Retrieved: 21 September 2007.
- ^ B-36 Deployment
- ^ Flying the Aluminum and Magnesium Overcast
- ^ Interview with B-36B 44-92075 Co-pilot 1st Lt R.P. Whitfield 1998, Retrieved: 24 September 2007.
- ^ Edmundson interview
- ^ B-36 Forum
- ^ Operation Castle: Report of Commander, Task Group 7.1 p. 24 (extract version), dated 1 February 1980], Retrieved: 23 September 2007.
- ^ Miller and Cripliver 1978, pp. 366, 369.
- ^ Lockett, Brian. Parasite Fighter Programs: Project Tom-Tom. Goleta Air and Space Museum. Retrieved: 3 February 2007.
- ^ Yenne 2004, p. 149.
- ^ a b B-36 wrecks
- ^ Synopsis of the Air Force Accident Report for RB-36H, 51-13722 posted 30 July 2003, Retrieved: 23 September 2007.
- ^ Ricketts, Bruce. Broken Arrow, A Lost Nuclear Weapon in Canada. Mysteries of Canada, 11 January 2006. Retrieved: 17 August 2007.
- ^ Doomsday
- ^ National Museum of the USAF factsheet about the YB-60
- ^ Air Force Link XC-99 begins piece-by-piece trip to Air Force Museum by 1st Lt Bruce R. Hill Jr., 433rd Airlift Wing Public Affairs, 22 April 2004.
- ^ Top of the World
- ^ Quote attributed to Captain Banda when he was escorting Air Cadet Michael R. Daciek, later Lieutenant Colonel Daciek, on an inside tour of the XC-99 in 1953.
Daciek, Michael R. B-36 Peacemaker/Ten Engine Bomber. YourHub.com 13 December 2006. Retrieved: 3 April 2008.
- Ford, Daniel. “B-36: Bomber at the Crossroads”. Air and Space/Smithsonian, April 1996. Retrieved: 3 February 2007.
- Jacobsen, Meyers K. Convair B-36: A Comprehensive History of America’s “Big Stick”. Atglen, Pennsylvania: Schiffer Military History, 1997. ISBN 0-7643-0974-9.
- Jacobsen, Meyers K. Convair B-36: A Photo Chronicle. Atglen, Pennsylvania: Schiffer Military History, 1999. ISBN 0-7643-0974-9.
- Jacobsen, Meyers K. “Peacemaker.” Airpower, Vol. 4, No. 6. November 1974.
- Jacobsen, Meyers K. and Ray Wagner. B-36 in Action (Aircraft in Action Number 42). Carrollton, TX: Squadron/Signal Publications Inc., 1980. ISBN 0-89747-101-6.
- Jenkins, Dennis R. Convair B-36 Peacemaker. St. Paul, Minnesota: Specialty Press Publishers and Wholsalers, 1999. ISBN 1-58007-019-1.
- Jenkins, Dennis R. B-36 Photo Scrapbook. St. Paul, Minnesota: Specialty Press Publishers and Wholesalers, 2003. ISBN 1-58007-075-2.
- Jenkins, Dennis R. Magnesium Overcast. St. Paul, Minnesota: Voyageur Press, 2001. ISBN 1-58007-042-6.
- Johnsen, Frederick A. Thundering Peacemaker, the B-36 Story in Words and Pictures. Tacoma, WA: Bomber Books, 1978. ISBN 1-55046-310-1.
- Leach, Norman S. Broken Arrow: America’s First Lost Nuclear Weapon. Calgary, Alberta: Red Deer Press, 2008. ISBN 978-0889953482.
- Miller, Jay and Roger Cripliver. “B-36: The Ponderous Peacemaker.” Aviation Quarterly, Vol. 4, No. 4, 1978.
- Morris, Lt. Col. (ret.) and Ted Allan. Flying the Aluminum and Magnesium Overcast. The collected articles and photographs of Ted A. Morris, ©2000.  Retrieved: 4 September 2006.
- Orman, Edward W. “One Thousand on Top: A Gunner’s View of Flight from the Scanning Blister of a B-36.” Airpower, Vol. 17, No. 2, March 1987.
- Pyeatt, Don. B-36: Saving the Last Peacemaker (Third Edition). Fort Worth, Texas: ProWeb Publishing, 2006. ISBN 0-9677593-2-3.
- Shiel, Walter P. The B-36 Peacemaker: “There Aren’t Programs Like This Anymore”.
- Taylor, John W.R. “Convair B-36.” Combat Aircraft of the World from 1909 to the present. New York: G.P. Putnam’s Sons, 1969. ISBN 0-425-03633-2.
- Wagner, Ray. American Combat Planes. New York: Doubleday & Company, Inc., 1968. ISBN 0-385-04134-9.
- Winchester, Jim. “Convair B-36”. Military Aircraft of the Cold War (The Aviation Factfile). Rochester, Kent, UK: The Grange plc., 2006. ISBN 1-84013-929-7.
- Wolk, Herman S. Fulcrum of Power: Essays on the United States Air Force and National Security. Darby, Pennsylvania: Diane Publishing, 2003. ISBN 1-42899-008-9.
- Yenne, Bill. “Convair B-36 Peacemaker.” International Air Power Review, Vol. 13, Summer 2004. London: AirTime Publishing Inc., 2004. ISBN 1-880588-84-6.
- Cowtown.net: Portal to B-36 resources
- Encyclopedia of American Aircraft
- XB-36 page on USAF National Museum web site
- B-36A page on USAF National Museum web site
- Aerospaceweb, with technical info and many pictures
- “Lt. Gen. James Edmundson interview transcript: Flying B-36 and B-47 planes.“. Race For the Superbomb. PBS Online
- B-36 operations Walker AFB Roswell New Mexico 1955-1957
- Very high resolution panoramic photograph of the bomb bay of the USAF National Museum’s B-36J