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23-585: The design was originally intended to be a relatively simple upgrade to the F-84 Thunderjet to make it more competitive with the F-86 Sabre , differing largely in the use of a swept-wing and tail. Given the small number of changes, it was assigned the next model letter in the F-84 series, F. The prototypes demonstrated a number of performance and handling issues, which resulted in marginal improvement over

46-553: A brief period using ex-French examples, the Israeli Air Force . In 1948, a swept wing version of the F-84 was created with the hope of bringing performance to the level of the F-86 . The last production F-84E was fitted with a swept tail, a new wing with 38.5 degrees of leading edge sweep and 3.5 degrees of anhedral , and a J35-A-25 engine producing 5,300 pound-force (23.58 kN) of thrust . The aircraft

69-408: A different canopy which opened up and back instead of sliding to the rear (a unique design, the canopy was mounted on a pair of hydraulic rams and a pivoted lever arm that allowed it to lift up and backwards while remaining almost level with the fuselage, instead of the more common simple hinged canopy), as well as airbrakes on the sides of the fuselage instead of the bottom of the aircraft. The aircraft

92-540: A front-line design was brief; it began to be moved to secondary roles as early as 1958. F-84Fs were then offered to NATO member countries and other allies, who took them up in large numbers. Operators included the Belgian Air Force , Royal Danish Air Force , French Air Force , West German Air Force , Hellenic Air Force , Italian Air Force , Royal Netherlands Air Force , Royal Norwegian Air Force , Republic of China Air Force , Turkish Air Force , and for

115-514: A periscope to give the pilot better visualization of the target, and a voice recorder to let the pilot narrate his observations. Being largely identical to the F-84F, the Thunderflash suffered from the same production delays and engine problems, delaying operational service until March 1954. The aircraft was retired from active duty in 1957, only to be reactivated in 1961, and finally retired from

138-727: A result, the F-84F was not declared operational until 12 May 1954. The second YF-84F prototype was completed with wing-root air intakes. These were not adopted for the fighter due to loss of thrust. However, this arrangement permitted placement of cameras in the nose and the design was adopted for the RF-84F Thunderflash reconnaissance version. The first YRF-84F was completed in February 1952. The aircraft retained an armament of four machine guns and could carry up to fifteen cameras. Innovations included computerized controls which adjusted camera settings for light, speed, and altitude,

161-601: The Air National Guard . The last RF-84F Thunderflash retired from the ANG in 1971. Three Hellenic Air Force RF-84Fs that were retired in 1991 were the last operational F-84s. Data from Fighters of the United States Air Force, Combat Aircraft since 1945 General characteristics Performance Armament Avionics Communications Equipment Richard Bach , who later wrote

184-521: The ANG in 1972. Several modified Thunderflashes were used in the FICON project . The Thunderstreak suffered from the same poor takeoff performance as the straight-wing Thunderjet despite having a more powerful engine. In reality, almost 700 pounds-force (3.11 kN) or ten percent of total thrust was lost because the J65 was installed at an angle and its jet pipe was not perfectly straight (in addition to

207-564: The F-84F utilized press-forged wing spars and ribs. At the time, only three presses in the United States could manufacture these, and priority was given to the Boeing B-47 Stratojet bomber over the F-84. The YJ65-W-1 engine was considered obsolete and the improved J65-W-3 did not become available until 1954. When the first production F-84F finally flew on 22 November 1952, it differed from the service test aircraft. It had

230-711: The F-84F, two Turkish Air Force F-84F Thunderstreaks shot down two Iraqi Il-28 Beagle bombers that crossed the Turkish border by mistake during a bombing operation against Iraqi Kurdish insurgents. This engagement took place on 16 August 1962. The F-84F was retired from active service with the USAF in 1964, and replaced by the North American F-100 Super Sabre . The RF-84F was replaced by the RF-101 Voodoo in USAF units, and relegated to duty in

253-519: The J65 engine continued to suffer from flameouts when flying through heavy rain or snow. As the result of the problems, the active duty phaseout began almost as soon as the F-84F entered service in 1954, and was completed by 1958. Increased tensions in Germany associated with construction of the Berlin Wall in 1961 resulted in reactivation of the F-84F fleet. In 1962, the fleet was grounded due to

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276-476: The J65 had a vertically stretched fuselage, with the air intake attaining an oval cross-section. Production delays with the F-84F forced the USAF to order a number of straight-wing F-84Gs as an interim measure. Production quickly ran into problems. Although tooling commonality with the Thunderjet was supposed to be 55 percent, in reality only fifteen percent of tools could be reused. To make matters worse,

299-748: The Soviet fighters were available during the ongoing Cold War for filming. They were painted a flat gray with red star insignia. Related development Aircraft of comparable role, configuration, and era Armstrong Siddeley Sapphire Too Many Requests If you report this error to the Wikimedia System Administrators, please include the details below. Request from 172.68.168.237 via cp1104 cp1104, Varnish XID 210313737 Upstream caches: cp1104 int Error: 429, Too Many Requests at Thu, 28 Nov 2024 07:47:30 GMT Pitch-up Too Many Requests If you report this error to

322-575: The air intake to be modified. With these and other changes, the design was finally ready to enter production, but only a fraction of the original production systems could be used and the aircraft was effectively a new design. It finally entered service in November 1954, by which time the Sabre had also undergone many upgrades and the Thunderstreak was relegated to the fighter-bomber role. Its time as

345-454: The airplane. In addition, spins in the F-84F were practically unrecoverable and ejection was the only recourse below 10,000 feet (3,000 m). Project Run In completed operational tests in November 1954 and found the aircraft to be to USAF satisfaction and considerably better than the F-84G. However, ongoing engine failures resulted in the entire fleet being grounded in early 1955. Also,

368-637: The appearance of the Republic F-105 Thunderchief , which used wing-root mounted air intakes of a similar design to those fitted on the RF-84F, the photorecon variant Thunderflash became known as the Thud's Mother . The earlier F-84A had been nicknamed the "Hog" and the F-84F "Super Hog," the F-105 becoming the "Ultra Hog". In what is probably one of the very few air-to-air engagements involving

391-562: The bestseller Jonathan Livingston Seagull , was an ANG F-84F pilot who was once activated for duty in Europe. His first book, Stranger to the Ground , described in detail what it was like to fly the Thunderstreak in the course of an operational flight at night from England to France in adverse weather. F-84Fs were also used to represent North Korean MiG-15 fighters in the 1958 film version of James Salters' novel "The Hunters", because none of

414-401: The corrosion of control rods. A total of 1,800 man hours were expended to bring each aircraft to full operational capacity. Stress corrosion eventually forced the retirement of ANG F-84Fs in 1971. On 9 March 1955, Lt. Col. Robert R. Scott , in a F-84F Thunderstreak, set a three-hour, 44-minute and 53-second record for the 2,446 miles (3,936 km) flight from Los Angeles to New York. With

437-475: The previous versions. Production was repeatedly delayed and another run of the straight-wing Thunderjets were completed as the G models. Looking for a clear performance edge compared to the G models, the engine was upgraded to the much more powerful British Armstrong Siddeley Sapphire built in the United States as the Wright J65 . The larger engine required the fuselage to be stretched into an oval shape and

460-507: The straight-wing Thunderjet with over 55 percent commonality in tooling. In the meantime, the USAF, hoping for improved high-altitude performance from a more powerful engine, arranged for the British Armstrong Siddeley Sapphire turbojet engine to be built in the United States as the Wright J65 . To accommodate the larger engine, YF-84F s with a British-built Sapphire as well as production F-84Fs with

483-465: The usual thrust losses from the long jet pipe). On a hot day, 7,500 feet (2,285 m) of runway were required for takeoff roll. A typical takeoff speed was 160 knots (185 mph, 300 km/h). Like the Thunderjet, the Thunderstreak excelled at cruise and had predictable handling characteristics within its performance envelope. Like its predecessor, it also suffered from accelerated stall pitch-up and potential resulting separation of wings from

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506-480: Was considered not ready for operational deployment due to control and stability problems. The first 275 aircraft, equipped with conventional stabilizer-elevator tailplanes, suffered from accelerated stall pitch-up and poor turning ability at combat speeds. Beginning with Block 25, the problem was improved upon by the introduction of a hydraulically powered one-piece stabilator . A number of aircraft were also retrofitted with spoilers for improved high-speed control. As

529-585: Was designated XF-96A . It flew on 3 June 1950 with Oscar P. Haas at the controls. Although the airplane was capable of 602 knots (693 mph, 1,115 km/h), the performance gain over the F-84E was considered minor. Nonetheless, it was ordered into production in July 1950 as the F-84F Thunderstreak . The F-84 designation was retained because the fighter was expected to be a low-cost improvement of

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