F-84F Thunderstreak

Infobox Aircraft
name=F-84F Thunderstreak RF-84F Thunderflash
type=Fighter-bomber
manufacturer=Republic Aviation


caption= USAF F-84F Thunderstreak
designer=Alexander Kartveli
first flight=
introduced=
retired=1972 US ANG 1991 Greece
status=
primary user=United States Air Force
more users=
produced=
number built=
unit cost=US$769,330 (F-84F)
developed from= F-84 Thunderjet
variants with their own articles= XF-84H Thunderscreech

The Republic F-84F Thunderstreak was an American-built swept-wing turbojet fighter-bomber. While an evolutionary development of the straight-wing F-84 Thunderjet, the F-84F was a new design. The RF-84F Thunderflash was a photo reconnaissance version.

Design and development

In 1949, Republic created a swept wing version of the F-84 hoping to bring performance to the F-86 level. 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.Knaack, Marcelle Size. "Encyclopedia of US Air Force Aircraft and Missile Systems: Volume 1 Post-World War II Fighters 1945-1973". Washington, DC: Office of Air Force History, 1978. ISBN 0-912799-59-5. The aircraft was designated XF-96A. It flew on 3 June 1950 with Otto 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 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-84Fs with a British-built Sapphire as well as production F-84Fs with the J65 had a vertically stretched fuselage, with the air intake attaining an oval cross-section. Production delays with the F-84F forced 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 15 percent of tools could be reused. To make matters worse, 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 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 a different canopy which opened up and back instead of sliding to the rear, as well as airbrakes on the sides of the fuselage instead of the bottom of the aircraft. The aircraft was considered not ready for operational deployment due to control and stability problems. Since early aircraft suffered from accelerated stall pitch-up, F-84F-25-RE introduced an all-moving tailplane. A number of aircraft were also retrofitted with spoilers for improved high-speed control. As a result, the F-84F was not declared operational until 12 May 1954.

Operational history

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, 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 corrosion of control rods. A total of 1,800 man hours was expended to bring each aircraft to full operational capacity. The aircraft were retired from active service in 1964. Stress corrosion forced retirement of ANG F-84Fs in 1971.

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, 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 the ANG in 1972.

Several modified Thunderflashes were used in the FICON project.

Flying the Thunderstreak

The Thunderstreak suffered from the same poor takeoff performance as the straight-wing Thunderjets in spite of having a more powerful engine. In reality, almost 700 pounds-force (3.11 kN) or 10 percent of total thrust was lost because the J65 was installed at an angle and its exhaust had a prominent kink. On a hot day, 7,500 feet (2,285 m) of runway were required for takeoff roll.Higham, Robin and Carol Williams. "Flying Combat Aircraft of USAAF-USAF (Vol.2)". Rockville, Maryland: Air Force Historical Foundation, 1978. ISBN 0-8138-0375-6.] 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 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).

With the appearance of the F-105 Thunderchief, the Thunderstreak became known as the Thud's Mother.

By the mid-1960s, the F-84F was replaced by the F-100 Super Sabre and the RF-84F by the RF-101 Voodoo in USAF units, being relegated to duty in the Air National Guard. The last F-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.

Richard Bach, who later wrote 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 great detail what it was like to fly the Thunderstreak.

Variants

;YF-84F: Two swept-wing prototypes of the F-84F, initially designated YF-96.;F-84F Thunderstreak: Swept wing version with Wright J65 engine. Tactical Air Command aircraft were equipped with Low-Altitude Bombing System (LABS) for delivering nuclear bombs. 2,711 built, 1,301 went to NATO under Mutual Defense Assistance Program (MDAP).;GRF-84F: 25 RF-84Fs were converted to be carried, and launched from the bomb bay of a GRB-36F bomber as part of the FICON project. The aircraft were later redesignated RF-84K.;RF-84F Thunderflash: Reconnaissance version of the F-84F, 715 built.;XF-84H: Two F-84Fs were converted into experimental aircraft. Each was fitted with a Allison XT40-A-1 turboprop engine of 5,850 shaft horsepower (4,365 kW) driving a supersonic propeller. Ground crews dubbed the XF-84H the Thunderscreech due to its extreme noise level.;YF-84J: Two F-84Fs were converted into YF-84J prototypes with enlarged nose intakes and a deepened fuselages for the General Electric J73 engine; the YF-84J reached Mach 1.09 in level flight on 7 April 1954. The project was cancelled due to the excessive cost of conversion of existing F-84Fs.

Operators

;BEL
*Belgian Air Force (197 x F-84F, 34 x RF-84F operated from 1955);ROC ;DNK;FRA;GER;GRE;IRN;ITA;NLD;NOR;POR;TUR;USA
*United States Air Force;YUG

pecifications (F-84F)

aircraft specifications

plane or copter?=plane
jet or prop?=jet
ref=Fighters of the United States Air ForceDorr, Robert F. and David Donald. "Fighters of the United States Air Force". London: Temple Press Aerospace, 1990. ISBN 0-600-55094-X.]

crew=1
length main=43 ft 4¾ in
length alt=13.23 m
span main=33 ft 7¼ in
span alt=10.25 m
height main=14 ft 4¾ in
height alt=4.39 m
area main=325 ft²
area alt=30 m²
empty weight main=13,830lb
empty weight alt=5,200 kg
loaded weight main=lb
loaded weight alt=kg
max takeoff weight main=28,000 lb
max takeoff weight alt=12,701 kg
engine (jet)= Wright J-65-W-3
type of jet=turbojet
number of jets=1
thrust main=7,220 lbf
thrust alt=32.2 kN
max speed main=695 mph
max speed alt= 604 knots, 1,119 km/h
max speed more=at sea level
cruise speed main=
cruise speed alt=
range main=810 mi
range alt=704 nmi, 1,304 km
range more= combat radius with two droptanks
ferry range main=
ferry range alt=
ferry range more=
ceiling main=46,000 ft
ceiling alt=14,000 m
climb rate main=8,200 ft/min
climb rate alt=42 m/s
loading main=86 lb/ft²
loading alt=423 kg/m²
thrust/weight=
armament=
*6× .50 in (12.7 mm) Browning M3 machine guns,
*Up to 6,000lb (2,727 kg) of rockets and bombs, including one Mark 7 nuclear bomb
avionics=
*A-1CM or A-4 gunsight with APG-30 or MK-18 ranging radar

ee also

aircontent
related=
* F-84 Thunderjet
* XF-84H Thunderscreech
* RF-84K FICON
* XF-91 Thunderceptor
* F-105 Thunderchief
similar aircraft=
* Saab 32 Lansen
* Dassault Mystère
* de Havilland Venom
* Gloster Meteor
* Grumman F9F Panther
* Grumman F9F/F-9 Cougar
lists=
see also=

References

Notes

Bibliography

* Bowers, Peter M. and Enzo Angellucci. "The American Fighter". New York: Orion Books, 1987. ISBN 0-517-56588-9.
* Donald, David and Jon Lake, eds. "Encyclopedia of World Military Aircraft". London: AIRtime Publishing, 1996. ISBN 1-880588-24-2.
* Forrer, Frits T. "The Fun of Flying". Gulf Breeze, Florida: Holland's Glory, 1992. ISBN 0-9714490-3-1.
* Keaveney, Kevin. "Republic F-84/Swept-Wing Variants (Aerofax Minigraph, No 15)". London: Aerofax, 1987. ISBN 0-942548-20-5.
* Swanborough, Gordon and Peter M. Bowers. "United States Military Aircraft Since 1909". Washington, DC: Smithsonian, 1989. ISBN 0-87474-880-1.
* Wagner, Ray. "American Combat Planes, Third Enlarged Edition". New York: Doubleday, 1982. ISBN 0-385-13120-8.

External links

* [http://www.f84thunderjet.com/ F-84 Thunderjet]
* [http://www.edwards.af.mil/gallery/html_pgs/f-84-1.htm Edwards Air Force base F-84 site]