Republic F-84 Thunderjet / Thunderstreak / RF-84 Thunderflash

Republic F-84B Thunderjet

The first prototype Republic XP-84 made its maiden flight on 28 February 1946, powered by a General Electric J35 engine.

Fifteen YP-84A were built in 1946 for service trials; 45-59482 to 45-59496.

Republic YP-84A 45-50490

Dubbed ‘Thunderjet’, the straight-winged F-84 saw operational service in Korea from December 1950, first as an escort fighter to B-29 bombers and then in the ground attack role. The F-84G was developed to carry nuclear weapons for tactical warfare and was used by TAC and SAC; F-84Gs without nuclear weapon delivery systems were supplied to various NATO air forces and no less than 4,457 straight-wing Thunderjets were built.

F-84E Thunderjet

Although it shared the same generic designation number as the straight-winged F-84 Thunderjet, the Republic F-84F Thunderstreak was essentially a new aircraft. The prototype XF-84F was an F-84E Thunderjet fitted with 40 degree sweptback wing and tail, and longer, faired-in cockpit hood. It was powered by a 5200 lb Allison J-35-A-25 turbojet. When Curtiss-Wright acquired a license to build the Armstrong Siddeley Sapphire turbojet in America, Republic fitted an imported Sapphire in the YF-84F prototype which flew on 14 February 1951. The USAF ordered this aircraft into production, with a Wright-built J65 Sapphire, as the F-84F Thunderstreak.

Republic F-84 Thunderstreak Article

F-84F

The RF-84F served as the backbone of NATO tactical strike forces, operating with Belgium, France, Italy, Greece, the Netherlands, Turkey and West Germany.

Yugoslavian F-84Gs

On 10 March 1953, five days after a Polish pilot had defected with his MiG-15 to the Danish island of Bornholm, two Czechoslovakian MiG attacked two American F-84G Thunderjets over Regensburg in Bavaria. One of the Thunderjets was shot down by the 23mm and 37mm cannon of one of the MiGs. The pilot ejected safely over Czechoslovakian territory.

By 1955 the F-84F Thunderstreak was the standard U.S.A.F. fighter-bomber, replacing F-86 Sabres and F-84E and -G Thunderjets. Can carry the tactical atomic bomb, and can be carried itself by GRB-36 “mother-plane”. Versions carried by GRB-36 have anhedral (downswept) tailplane.

Initially conceived by Republic dating 1949, the Thunderstreak was first flown in prototype form as the YF-84F on 3 June 1950, this aircraft using a standard F-84E fuselage with a swept wing and being powered by a single Allison YJ35-A-25 engine rated at 2359-kg (5,200-lb) thrust. Early flight testing of this aircraft very quickly revealed that the performance left a great deal to be desired and it was therefore decided to incorporate the British Sapphire (Wright J65) engine, impetus for the change being largely provided by US involvement in the Korean War, although in the event the F-84F did not see action in that conflict. Adoption of the more powerful engine in turn necessitated some redesign and it was not until late 1952 that the first production specimen made its maiden flight. Altogether 2,711 F-84Fs were built for service with allied nations from the late 1950s onwards.

F-84F

A specialized photo-reconnaissance derivative of the F-84 known as the RF84F Thunderflash was evolved more or less concurrently, this being most easily recognized by its revised air inlet layout which permitted the battery of cameras to be mounted in the extreme nose section. The RF-84F Thunderflash photo-reconnaissance aircraft had cameras in lengthened nose, only 4 guns, and wing-root air intakes. It too can be carried by GRB-36. The first prototype flew in February 1952. Including the prototype YRF-84F, 716 Thunderflashes were built, almost half of this figure being destined for overseas service under the terms of the Mutual Defense Aid Program, examples being supplied to Italy, Greece, West Germany, Turkey, the Netherlands, Belgium, Denmark, Taiwan, France and Norway.

It has another distinction so far as the USAF is concerned, being the aircraft with which flight refuelling techniques for fighters were developed.

RF-84F

A total of 4457 F-84 “Thunderjet” were built.

The second attempt to use the B 36 as an aircraft carrier took place in 1955 and 1956. Seeking a reconnaissance aircraft with sufficient range to reach the Soviet Union, the USAF came up with FICON, which stood for Fighter In CONvair. By hitching a Republic RF 84 Thunderflash to a B 36, the photo-reconnaissance jet’s range could be extended from 3220 km (2000 miles) to 19,310 km (12,000 miles). Some thought was also given to a nuclear bomb equipped Thunderstreak substituting for the Thunderflash. Twenty five RF 84Fs were modified for parasite duty. On a typical mission the mother ship B 36 would depart from Fairchild Air Force Base, Spokane, Washington to be joined in the air by an RF 84K (as the parasite Thunderflashes were designated) from Moses Lake Air Force Base. The fighter would be hoisted into the B 36’s bomb bay.

F-84G Thunderjet

The F-84G Thunderjet featured conventional ailerons, elevators, rudder and trailing edge flaps. An air-brake is under the centre fuselage. The tricycle undercarriage has a single wheel on each unit, the mains retracting inward into the wings, and nose-wheel retracts rearward.

Even in the mid-1950s the superiority of the jet powerplant for combat aircraft was questioned by some. A modern technology propeller driven by a turbine (a turboprop) offered high speeds, long endurance and low landing speeds. To test this concept the USAF commissioned two XF-84Hs from Republic.

XF-84H

Powered by the Allison XT-40 coupled turboprops driving a singe supersonic blade propellor, the noise the F-84H made has been described as an ‘unholy shriek’, leading to the nickname ‘Thunderscreech’. Resonance off the ground made groundcrew physically sick. The two aircraft only made a dozen test flights, all but two of which resulted in emergency landings and the USAF refused to accept it for their own tests, cancelling the programme in 1956.

The first XF-84H spent 40 years on a pole at Bakersfield Airport, California, its propeller slowly (and quietly) rotated by an electric motor.

Gallery

F-84E Thunderjet
Fighter-bomber
Engine: 5,000 lb. thrust Allison J35-A-17 turbojet.
Wingspan: 37 ft. 5 in
Length: 38 ft. 5 in
Loaded weight: 18,000 lb.
Max. speed: 630 m.p.h.
Ceiling: over 45,000 ft
Normal range: 1,700 miles
In flight refueling: yes
Armament: 6x.50 in. machine-guns
Bombload: 4 x 1,000 lb. bombs or up to 32 x 5 in. rockets.
Crew: 1

Republic F-84F Thunderstreak
Type: single-seat strike fighter
Powerplant: one 3275-kg (7,220-lb) thrust Wright J65-W-3 turbojet
Maximum speed 1118 km/h (695 mph) at sea level
Initial climb rate 2499 m (8,200 ft) per minute
Service ceiling 14020 m (46,000 ft)
Combat radius, clean 724 km (450 miles)
Ferry range 3444 km (2,140 miles)
Maximum take-off 12701 kg (28,000 lb)
Wingspan 10.26 m (33 ft 7¼ in)
Length 13.23 m (43 ft 4¾ in)
Height 4.39 m(14 ft4¾ in)
Wing area 30.19 sq.m (325 sq ft)
Armament: six 12.7-mm (0.5-in) M3 machine-guns
Bomb load, 2722 kg (6,000 lb)
Crew: 1

RF-84F Thunderflash
Engine: Wright J65-W-7, 7800 lb
Wingspan: 33 ft 7 in
Length: 47 ft 7.75 in
Height: 15 ft
Max speed: 679 mph at SL
Max ROC: 8000 fpm
Service ceiling: 46,000 ft
Max range: 2200 mi
Armament: 4 x .50 in mg

F-84G Thunderjet
Engine: 1 x Allison J35-A-29, 24.9kN / 5600 lb
Wingspan: 11.4 m / 37 ft 5 in
Length: 11.7 m / 38 ft 5 in
Height: 3.8 m / 12 ft 6 in
Wing area: 24.2 sq.m / 260.49 sq ft
Wheel track: 16 ft 6 in
Max take-off weight: 8455-10670 kg / 18640 – 23523 lb
Empty weight: 5033 kg / 11096 lb
Max. speed: 970 km/h / 603 mph
Cruise speed: 775 km/h / 482 mph
Ceiling: 12350 m / 40500 ft
Range w/max.fuel: 1680 km / 1044 miles
Armament: 6 x 12.7mm machine-guns
Bombload: 4500 lb
Crew: 1

XF-84H
Engine: 1 x 5850 hp Allison XT40-A-1 turboprop
Wingspan: 10.18 m / 33 ft 5 in
Length: 15.67 m / 51 ft 5 in
Height: 4.67 m / 15 ft 4 in
Max take-off weight: 8123 kg / 17908 lb
Max. speed: 837 km/h / 520 mph
Crew: 1

Republic F-84E Thunderjet
Republic F-84F Thunderstreak
RF-84F Thunderflash

Republic XP-72

The Republic XP-72 was based upon the P-47 airframe and was designed by Alexander Kartveli’s fighter team as a ‘Super Thunderbolt’ around the 3,000-hp / 2237kW Pratt & Whitney R-4360-13 Wasp Major radial engine. The powerplant was the most powerful piston engine to reach production in any country during World War II.

Intended primarily to be faster than the Thunderbolt, the XP-72 was viewed in part as a remedy for the Third Reich’s high-speed V-l buzz bomb. The USAAF planned to use the fighter to intercept buzz bombs, with a maximum speed of 490mph and an initial climb rate of 3,100ft/min the XP-72 could reach 6000m / 20,000 ft in just under five minutes. Operational P-72s would have been armed with six .50-calibre (12.7-mm) guns.

The first of two examples flew at Farmingdale on 2 February 1944 using a large four-bladed propeller. The second XP-72 flew in July 1944 with the intended Aeroproducts six-bladed contra-rotating propeller. The second aircraft, however, was lost on an early flight.

With priority shifted to long-range escort fighters, this promising interceptor was not needed. Even with a range of 1,200 miles, the XP-72 failed to get a production order. The other XP-72 airframe is thought to have been scrapped at Wright Field around VJ-Day.

Engine: Pratt & Whitney R-4360-13 Wasp Major, 3,000-hp
Max take-off weight: 6690 kg / 14749 lb
Empty weight: 4973 kg / 10964 lb
Wingspan: 12.49 m / 41 ft 0 in
Length: 11.17 m / 37 ft 8 in
Height: 4.42 m / 15 ft 6 in
Wing area: 27.87 sq.m / 299.99 sq ft
Max. speed: 788 km/h / 490 mph
Ceiling: 12800 m / 42000 ft
Range: 1930 km / 1199 miles
Armament: 6 x 12.7mm machine-guns, 2 x 450kg bombs

Republic XP-72

Republic SPA / AT-12

From its P-35 single-seat tighter Republic (latterly Seversky) developed the Model 2PA Guardsman two-seat escort fighter and fighter-bomber with the same type of rearward semi-retracting main landing gear units and the glazed rear portion of the cockpit expanded rearward to accommodate the second crewman. There was no US market for such an aeroplane, so the company looked for export sales.

Two were sold to the USSR as 2PA-L/As, 20 2PA-B3s went to Japan with the local designation A8V1, and 52 2PA-204Ls were ordered by Sweden to supplement her J 9 fighters (P-35s sold with the company designation EP-1-06s). Early in World War II the US administration embargoed the delivery of the 2PA-204Ls to Sweden, and these were taken into the USAAC inventory as AT-12 advanced fighter trainers with the designation AT-12. The aircraft saw limited use in this role during the first part of World War II.

AT-12
two-seat advanced tighter trainer
Span: 12.5m (41ft )
Length: 8.43m (27 ft 8in)
Powerplant: 1 x Pratt & Whitney R-1830-45, 783kW (1,050 hp)
Armament: 4 or 7 x 7.62-mm (0.3-in) mg
Bombload: 227 kg (500 lb) under wings
Max T/O weight: 2918 kg (6,433 lb)
Max speed: 285 mph at 10,000ft
Operational range: 1,200 miles

Republic P-43 Lancer

The Lancer was a single-seat interceptor fighter that first appeared in service evaluation YP-43 form in 1940. With a Pratt & Whitney R-1830 Twin Wasp radial engine and bulky fuselage, it was clearly a product of the Republic Aviation Corporation. Production for the USAAF, RAAF and China totalled 272 aircraft in three versions. Six P-43B reconnaissance fighters were allotted for Australian RAAF use, as PRU aircraft.

The P-43 Lancer design was developed further into the P-47 Thunderbolt.

P-43
Engine: 1 x Pratt-Whitney R-1830-47, 1167kW
Length: 8.69 m / 29 ft 6 in
Height: 4.27 m / 14 ft 0 in
Wing area: 20.72 sq.m / 223.03 sq ft
Max take-off weight: 3600 kg / 7937 lb
Empty weight: 2565 kg / 5655 lb
Wingspan: 10.97 m / 36 ft 0 in
Max. speed: 562 km/h / 349 mph
Ceiling: 11580 m / 38000 ft
Range: 1287 km / 800 miles
Crew: 1
Armament: 2 x 12.7mm machine-guns, 2 x 7.62mm machine-guns

Republic P-43 Lancer

Replica Plans SE-5A

The 5/6th scale replica was designed as an easy and inexpensive representation of this famous First World War Fighter using modern materials and engines. The reduced scale allows for the use of 65 to 100 hp “flat four” engines although some examples have more powerful engines. Wood and fabric construction.

The prototype flew in Canada in 1970 and there were two flying in New Zealand with at least two more under construction. The wooden wing has a leading edge covered with either fibreglass or aluminum, the rest being fabric-covered. The plywood-covered box fuselage has a fabric-covered turtle-deck and aluminum-covered forward section. Performance from an 85 hp powered SE-5A Replica are a cruise speed of 135 km/h and 150 m/min climb rate.

Dec 73

Gallery

Engine: Continental O-200, 100 hp
HP range: 85-125
Height: 7.67 ft
Length: 18.18 ft
Wing span: 23.33 ft
Wing area: 146 sq.ft
Fuel cap: 18 USG
Weight empty: 750 lb
Gross: 1150 lb
Speed max: 110 mph
Cruise: 80 mph
Range: 250 sm
Stall: 35 mph
ROC: 900 fpm
Take-off dist: 400 ft
Landing dist: 550 ft
Service ceiling: 10,000 ft
Seats: 1
Landing gear: tail wheel

Renard & Krebs La France / Chalais-Meudon La France

In 1884, under the direction of Renard and Krebs of the French army aeronautical establishment at Chalais Meudon, successful experiments were made employing electrical power with the airship La France.

At the French military balloon establishment at Chalais Meudon, in 1884, engineers Charles Renard and Captain A.C.Krebs designed and constructed the airship La France which was to prove capable of steady, navigable flight, and eas able to describe circular flights against the wind and return to its departure point.

La France, with a capacity of 66,000 cu.ft, was 165 ft long with a diameter of 28 ft, the envelope being made from Chinese varnished silk and of streamlined form. Below the envelope an enclosed car, 108 ft in length, contained a Gramme electric motor, developing 8.5-9 hp for a weight of 210 lb, together with the chromium-chloride batteries that drives a cloth covered tractor airscrew of 23 ft diameter. The battery weighed 435 kg.

The France was thirty-two feet in maximum diameter and nearly 200 feet long, the empennage planes aggregating about 400 square feet were placed forward of the stern.

Steering in the horizontal plane was effected by a large rectangular rudder at the stern, while vertical movement and attitude were controlled by a sliding weight mounted within the body of a car assistd by an ‘elevating rudder’.

In a series of trials the airship demonstrated controlled flight, achieved a speed of 14 mph and made several flights over Paris. The weight of the batteries, limited range and carrying capacity prevented further development.

The first trial of La France took place on 9 April 1884. The flight proving a limited success: making a circular flight of 5 miles in twenty-three minutes at a speed of around 12.5 mph in still air, then returning to its starting point, Chalais-Meudon – the first time this had ever been done. Six other flights were made during 1884-85, including two over Paris.

Chalais-Meudon Renard-Krebs “La France”
Engine: 1 x Elektromoteur Gramme electric: 9 hp
Batteries: Chromium chloride
Contained volume: 65,695 cu.ft / 1860 cu.m
Length: 165 ft / 50.0 m
Width of hull: 27.887 ft / 8.5 m
Height: 60 ft
Gross lift: 2.0 ton
Useful lift: 0.1 ton
Max. speed: 13 mph / 11 kt / 20 km/h
Crew: 3

Renard R-38

Developed in parallel with the R-37, the R-38 was essentially similar to the R-36 apart from having a 1030hp Rolls-Royce Merlin II engine. It was originally proposed with wings of two different sizes, but the sole prototype retained a similar wing to that of the R-36 and R-37. Armament comprised four wing-mounted 7.7mm or 13.2mm machine guns.

The R-38 flew for the first time on 4 August 1939, and gave excellent results during its test programme, which was still in process when German forces occupied Belgium. The sole prototype was flown to Bordeaux when the final collapse of Belgian resistance became inevitable, but was scrapped after capture in France by German forces.

Max take-off weight: 2600 kg / 5732 lb
Empty weight: 1950 kg / 4299 lb
Wingspan: 11.64 m / 38 ft 2 in
Length: 8.80 m / 29 ft 10 in
Height: 2.90 m / 10 ft 6 in
Wing area: 20.00 sq.m / 215.28 sq ft
Max. speed: 545 km/h / 339 mph
Range: 1350 km / 839 miles

Renard R-37

With an airframe fundamentally similar to that of the R-36, the R-37 differed primarily in having a close cowled 1100hp Gnome-Rhone 14N-21 14-cylinder radial engine. Cooling air reached the engine via a narrow annulus, was mixed with exhaust gases and ejected through two groups of nozzles to provide some thrust augmentation.

The proposed armament consisted of four 7.7mm or two 13.2mm machine guns mounted in the wings.

Although the R-37 was displayed statically at the Salon de Bruxelles in July 1939, no attempt had been made to fly this prototype before the German occupation of Belgium in May 1940. The R-37 was discovered at Evere by the occupation forces and a Luftwaffe pilot – possibly unaware that the aircraft had not previously been flown – flew the aircraft to Beauvechain. There is no record of any subsequent flight testing, although it is known that the R-37 was taken to Germany. Prior to the German occupation, Alfred Renard had prepared a project for a two-seat version, the R-37B, for use as a ground attack aircraft.

Max take-off weight: 2460 kg / 5423 lb
Empty weight: 1810 kg / 3990 lb
Wingspan: 11.64 m / 38 ft 2 in
Length: 8.40 m / 28 ft 7 in
Height: 2.90 m / 10 ft 6 in
Wing area: 20.00 sq.m / 215.28 sq ft
Max. speed: 510 km/h / 317 mph

Renard R-37