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The J 22 was a Swedish single-seater fighter aircraft developed in the mid-1940's. The J 22 was a low mid-wing cantilever monoplane of metal frame covered in plywood construction powered by a Pratt and Whitney Twin-Wasp two-row radial air-cooled engine providing a top speed of 575 kmh. The J 22 was produced in two variants, A and B, armed with two 13.2 mm and two 7.9 mm machine-guns in the wings, or four 13.2 mm machine-guns in the wings respectively.
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The Taylor Monoplane J.T.1 was a British amateur-designed single-seater ultra-light monoplane designed during the early 1960's to be very low-cost. The Taylor Monoplane J.T.1 was a low-wing cantilever monoplane powered by a JAP two-cylinder horizontally-opposed air-cooled engine providing a top speed of 167 kmh and a range of 370 km.
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The Taylor J.T.2 Titch was a British amateur-designed single-seater light monoplane first flown in 1967, shortly afterwards crashing on another prototype flight killing its designer, John Taylor. The Taylor J.T.2 Titch was a low-wing cantilever monoplane of wooden construction powered by a Continental C85-12F four-cylinder horizontally-opposed air-cooled engine.
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The Saab JA 37 is a Swedish single-seat all-weather interceptor fighter aircraft with secondary strike capability.
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Jabiru was a joint British-Australian unguided three-stage rocket test vehicle used for making studies of aerodynamic phenomena during the 1960's. The Jabiru Mk II was 125 cm long with a diameter of the first stage of 43 cm. Jabiru carried a 90 kg payload at a speed of 9300 km to an altitude of 290 km.
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The Saab JAS 39A (single-seater) and JAS 39B (dual-seater) 'Gripen' are Swedish multi-role fighter aircraft first flown in December 1988 and in operational service with the Swedish Air Force. The Gripen is equipped to carry an extensive range of air-to-air and air-to-surface weaponry, including rocket pods, stand-off dispenser weapons, short and medium range air-to-air missiles, Maverick missiles and an internally mounted Mauser 27 mm cannon. The Gripen has seven external hard points for carrying payloads, one at each wingtip, two under each wing and one on the fuselage centreline. Sidewinder AIM-9L air-to-air missiles are mounted on the wingtips Anti-ship missiles include the radar guided Saab RBS15F and the Maverick missile. The air-to-air missiles include MICA and the AIM-120B.
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The British Aerospace Jet Provost is a British two-seater primary/basic flying trainer aircraft that entered service in 1959. The British Aerospace Jet Provost is powered by a Rolls-Royce Viper ASV.11 Mk 202 turbojet providing a top speed of 708 kmh and a range of 1450 km with tip tanks.
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The Handley Page HP 137 Jetstream 31 is a British light corporate transport and regional airliner. The Jetstream 31 is a low-wing cantilever monoplane powered by two Turbomeca Astazou XVID turboprops providing a top speed of 555 kmh and a range of 2224 km. The Jetstream 31 carries a crew of two plus a stewardess and is fitted with between four and eighteen passenger seats.
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The Jetstream 31ez is an inshore maritime patrol version of the Jetstream 31. It is fitted with 360 degree radar and a search light and carries a crew of five.
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The Handley Page Jetstream T.Mk1 is a British military variant of the Jetstream 20 that entered military service in 1973 as a multi-engine pilot trainer aircraft. The Jetstream T.Mk1 is powered by two Turbomeca Astazou XVID turboprops providing a top speed of 555 kmh and a range of 2224 km. The
Jetstream T.Mk1 carries a crew of two - pupil and instructor - and up to four passengers.
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The Jindivik was an Australian, large, pilotless, radio controlled weapons target aircraft widely used by the British and Australian armed forces during the 1960's. Design of the Jindivik was started in 1948 and the prototype first flown in 1952. The Jindivik was a mid-wing cantilever monoplane of aluminium alloy construction powered by a Bristol Siddeley Viper Mk 201 turbojet engine providing a top speed of 908 kmh and a maximum range of 1320 km depending upon the fitted equipment. Typically the Jindivik was fitted with cameras in pods forward of the wing leading-edges, near the wing-tips to film the approach and proximity of missiles fired against the target. Generally the Jindivik was used as a tug towing a target, and many were flown in North Wales during the 1960's.
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The Oberlerchner JOB 15 is a series of Austrian four-seater light monoplanes first flown in 1960, production starting in 1961. The JOB 15-150, first produced in 1963 replacing the initial JOB 15-135, is a low-wing cantilever monoplane powered by a Lycming O-320-A2B four-cylinder horizontally-opposed air-cooled engine providing a top speed of 235 kmh and a range of 1000 km.
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The Jodel D11 was a French two-seater dual-control version of the Jodel D9 Bebe aircraft. The Jodel D11 was a low-wing cantilever monoplane powered by a Salmson radial engine providing a top speed of 170 kmh and a range of 600 km.
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The Jodel D111 is a French two-seater, dual-control light monoplane. The Jodel D111 is a low-wing cantilever monoplane, the same as the Jodel D11, but powered by a Minie flat-four engine providing a top speed of 200 kmh and a range of 700 km.
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The Jodel D112 Club was a French two-seater, dual-control light monoplane based upon the Jodel D11 but powered by a Continental engine. The Jodel D112 was a low-wing cantilever monoplane powered by a Continental flat-four engine providing a top speed of 180 kmh and a range of 530 km.
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The Aero-Difusion Jodel D1190 Compostela is a Spanish two-seater light cabin monoplane developed from the French Jodel D119 during the early 1960's. The Jodel D1190 is a low-wing cantilever monoplane powered by a Rolls-Royce/Continental C90-14F four-cylinder horizontally-opposed air-cooled engine providing a top speed of 230 kmh and a range of 1100 km.
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The Jodel D140 Mousquetaire is a French four-seater touring light aircraft first flown as a prototype in 1958. The Jodel D140E Mousquetaire V is a low-wing cantilever monoplane powered by a Lycoming O-360-A2A four-cylinder horizontally-opposed air-cooled engine providing a top speed of 250 kmh and a range of 1400 km. The Jodel D140 can also be used as an ambulance, carrying a single stretcher in the cabin instead of passengers.
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The Jodel D140R Abeille is a French light aircraft developed from the Jodel D140 Mousquetaire as a glider and banner towing version. The Jodel D140R Abeille is a low-wing cantilever monoplane powered by a Lycoming O-360-A2A four-cylinder horizontally-opposed air-cooled engine providing a top speed of 250 kmh and a range of 1400 km.
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The San Jodel D150 Mascaret is a French two-seater, side-by-side light aircraft developed as a replacement for the Jodel D112 and was first flown as a prototype in 1962. The San Jodel D150 Mascaret is powered by a Rolls-Royce/Continental O-200-A engine providing a top speed of 241 kmh and a range of 1610 km.
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The Jodel D9 Bebe is a French single-seater light monoplane of spruce and plywood construction, first flown in 1948. The Jodel D9 Bebe is a low-wing cantilever monoplane powered by a Volkswagen flat-four engine providing a top speed of 150 kmh and a range of 460 km.
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The Centre Est Jodel Sicile Record was a French three/four seater light aircraft developed from the Jodel Ambassadeur during the 1960's. The Jodel Sicile Record was a low-wing cantilever monoplane of wooden construction powered by a Continental O-200A (model DR1050) or Potez 4 E-20 (model DR1051) four-cylinder horizontally-opposed air-cooled engine providing a top speed of 230 and 255 kmh respectively. A Jodel Sicile Record won the 1964 circuit of Sicily race at an average speed of 272 kmh.
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The Jovair J-2 was an American side-by-side two-seat light autogyro flown for the first time as a prototype in 1962. The Jovair J-2 was powered by a Lycoming O-360-A2E four-cylinder horizontally-opposed air-cooled engine providing a top speed of 193 kmh and a range of 560 km.
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The Jovair Sedan 4E was an American four-seat tandem rotor light helicopter first produced during the 1960's powered by a Franklin 6A-350 six-cylinder horizontally-opposed air-cooled engine providing a top speed of 145 kmh and a range of 400 km fully laden.
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The Kaminskas Papoose Jungster I was an American single-seat, amateur build sporting biplane designed as a scaled down replica of the Bucker Bu 133 Jungmeister biplane, and first flown in 1962. The Jungster I was a braced biplane of fabric-covered wooden construction powered by a Lycoming O-235-C four-cylinder horizontally-opposed air-cooled engine providing a top speed of 209 kmh and a range of 320 km.
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The Kaminskas Jungster II was an American single-seat parasol-wing, amateur build sporting monoplane first flown in 1966. The Jungster II was a strut-braced parasol-wing monoplane of fabric-covered wooden construction powered by a Lycoming O-360-A1A four-cylinder horizontally-opposed air-cooled engine providing a top speed of 257 kmh.
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The Junior Ace is an American amateur-build two-seater side-by-side ultra-light monoplane derived from the Baby Ace Model D ultralight monoplane. The Junior Ace is powered by a Continental C85 four-cylinder horizontally-opposed air-cooled engine providing a top speed of 209 kmh and a range of 560 km.
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The Junkers F-13 was a German passenger carrying aircraft. It entered service in 1919 and remained in use until the 1930s.
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The Junkers J4-10 was a two-seater low level fighter aircraft. It was the first all-metal aircraft built during the Great War.
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The Junkers Ju 188 was a German four-seat medium bomber of the Second World War. The Junkers Ju 188E-1 was powered by two 1700 hp BMW 801D-2 14-cylinder radial piston engines providing a top speed of 500 kmh and a range of 1945 km. Armaments consisted of one forward firing 20 mm MG 151 cannon in the nose, a 13 mm MG 131 machine-gun in the dorsal turret, a 13 mm MG 131 machine-gun in the rear of the cockpit canopy and a rearward-firing 7.92 mm MG 81 machine-gun in the lower front fuselage, and a bomb load of 3000 kg.
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The Junkers Ju 252 was a German transport and utility aircraft of the Second World War. Design work started on the Ju 252 in 1939, and the first prototypes were built in 1940, the first flying in October 1941, entering service in 1943 before being withdrawn in 1944. The Junkers Ju 252 had a top speed of 272 mph and a typical range of 3000 km. It was armed with a 13 mm MG 131 trainable machine-gun in a power operated EDL 131 dorsal turret and two 7.92 mm MG 15 trainable lateral-firing machine-guns in two beam positions. A crew of three were carried and the aircraft provided accommodation for 32 passengers or 2000 kg of freight.
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The Junkers Ju 288 was a German twin-engined bomber aircraft of the Second World War first flown in 1940 but only used operationally in very small numbers. The Junkers Ju 288 was developed in several versions, the
Junkers Ju 288C being intended as a day bomber and was powered by four BMW 801 L2 14-cylinder radial air-cooled engines providing a top speed of 448 kmh and a range of 3985 km. The Junkers Ju 288 carried a crew of three and was variously armed with machine-guns in the dorsal turret, tail and ventral blister and a bomb load of 4000 kg.
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The Junkers Ju 290 was a German long-range maritime reconnaissance bomber aircraft of the Second World War developed from the Junkers Ju 89. The Junkers Ju 290A-7 was powered by four 1700 hp BMW 801D 14-cylinder radial piston engines providing a top speed of 440 kmh and a range of 6090 km. Armaments consisted of one 20 mm MG 151 cannon in each of two dorsal turrets, one MG 151 cannon in the tail position, one MG 151 cannon in the glazed nose, one MG 151 cannon in a ventral gondola in the nose, two 20 mm MG 151 cannons in lateral positions, one 13 mm MG 131 machine-gun in a rear ventral gondola, and either a bomb load of 3000 kg or three Henschel Hs 293, 294 or FX-1400 Fritz-X guided missiles.
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The Junkers JU 352 (Herkules) was a German transport and utility aircraft of the Second World War, in service from 1944 to 1945. The Junkers JU352 was a low-wing cantilever monoplane powered by three BMW 323 R-2 9-cylinder radial air-cooled engines providing a cruising speed of 240 kmh and a typical range of 1800 km. It was armed with one 20 mm MG 151/20 trainable cannon in a power operated HD 151/2 dorsal turret, and provision for two 13 mm MG 131 trainable lateral-firing machine-guns in the beam positions. The aircraft accommodated 4300 kg of freight and a crew of five.
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The Junkers Ju 388 was a series of mainly abortive German developments of the Junkers Ju 88 during the Second World War and included a fighter - the Junkers Ju 388J; a bomber - the Junkers Ju 388K and a reconnaissance model - the Junkers Ju 388L. Only the reconnaissance aircraft made it into production, and then less than fifty were built.
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The Junkers Ju 388J was an abortive German all-weather fighter aircraft of the Second World War, the project being scrapped after three prototypes had been constructed.
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The Junkers Ju 388K was a German bomber version of aircraft of the Junkers Ju 388 family. The Junkers Ju 388K was powered by two BMW 801 G or Jumo 222 A/B or E/F or Jumo 213 E engines providing a top speed of 590 kmh and a range of 2140 km. Armaments consisted of twin MG 131 machine-guns in a remote-controlled tail-turret.
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The Junkers Ju 388L was a German three-seat photographic reconnaissance aircraft of the Second World War built between 1943 and 1944 when production was abandoned. The Ju 388L-1 was powered by two 1890 hp BMW 801TJ 14-cylinder radial piston engines providing a top speed of 615 kmh and a range of 3475 km when equipped with external tanks. Armaments consisted of a remotely- controlled FA15 tail barbette equipped with two 13 mm MG 131 machine-guns.
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The Junkers Ju 52 was a German medium bomber and troop transport aircraft of the Second World War produced from 1932 to 1944. The Ju 52 was powered by three 725 hp BMW 132A-3 9-cylinder radial piston engines providing a top speed of 275 kmh and a range of 1300 km when fitted with auxiliary tanks. Armaments consisted of a 7.92 mm MG 15 machine-gun in an open dorsal position and one in a retractable ventral position.
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The Junkers Ju 86 was a German bomber/reconnaissance aircraft and civilian passenger airliner of the Second World War. Early models were powered by two Jumo 205C engines providing a top speed of 175 mph and a range of 1500 km. Later models were powered by two BMW 132DC engines giving a top speed of 235 mph and a range of 1200 km. The Ju 86 was armed with three 7.92 mm MG 15 manually aimed machine-guns mounted in the nose, dorsal and retractable ventral positions and an internal bomb load of four 250 kg or sixteen 50 kg bombs. The civilian passenger variant carried ten passengers and a crew of three.
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The Junkers Ju 87 (Stuka) was a German single-engine dive bomber of the Second World War. It was powered by a 1000hp Jumo engine giving it a top speed of 242 mph.
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The Junkers Ju 87B-1 was a German fighter-bomber used during the Second World War. It was armed with two 7.9 mm MG 17 machine-guns in the wings, one 7.9 mm MG 15 machine-gun in the rear cockpit and it could carry a 1100lb bomb under the fuselage, or four 110lb bombs on the wings. It had a crew of two and a top speed of 217 mph. It had a range of 342 miles.
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The Junkers Ju 88C was a German night-fighter of the Second World War, originally designed as a high-speed bomber but the performance of the prototypes was so impressive that it was decided to use the aircraft as a heavy fighter. It had a top speed of 307 mph and a typical range of 1040 km. It was armed with three 20 mm MG 151/20 fixed forward-firing cannons one in the nose and two in the ventral tray, three 7.92 mm MG 17 fixed forward-firing machine-guns in the nose, two 20 mm MG 151/20 obliquely upward and forward-firing cannons in the central fuselage and one 13 mm MG 131 trainable rearward-firing machine-gun in the rear of the cockpit.
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The Junkers Ju 88G was a German night-fighter of the Second World War, entering service in 1944 as an improvement upon the Junkers Ju 88C. The maximum speed was increased to 389 mph and the armaments were amended to four 20 mm MG 151/20 forward-firing cannons in the ventral tray, two 20 mm MG 151/20 obliquely upward and forward-firing cannons in the rear fuselage and one 13 mm MG 131 trainable rearward-firing machine-gun in the rear of the cockpit.
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The Junkers W34 was a German single-engine commercial transport plane developed in 1926 and adopted by the Luftwaffe during the Second World War as a navigational trainer and light transport aircraft. The Junkers W34hi was powered by a 600 hp BMW 132A 9-cylinder radial engine providing a top speed of 265 kmh and a range of 900 km. It could carry a pay load of 1500 kg, typically six seated passengers.
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The Jurca MJ2 Tempete is a French single-seater light monoplane first flown as a prototype in 1956, and designed to be distributed in kit form to amateur builders around the world. The Jurca MJ2 Tempete is a low-wing cantilever monoplane of wooden construction powered by a Continental A65 four-cylinder horizontally-opposed air-cooled engine providing a top speed of 193 kmh and an endurance of three hours and twenty minutes flying time.
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The Jurca MJ3 is a French single-seater sporting aircraft formed from the fuselage of the Jurca MJ2 Tempete with different wings attached, the new wings having an extended leading-edge inboard of the fence on each side and a redesigned tip shape. The Jurca MJ3 is powered by various flat-four engines of between 85 and 125 hp, the standard engine being the Continental C90 providing a cruising speed of 210 kmh.
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The Jurca MJ4 is a French single-seater sporting aircraft formed from the Jurca MJ3 with a sweptback fin and rudder. The Jurca MJ4 has a cruising speed of 215 kmh.
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The Jurca MJ5 Sirocco is a French two-seater monoplane developed from the Jurca MJ2 Tempete as a club training and touring aircraft, and first flown in 1962. The Jurca MJ5 Sirocco is a low-wing cantilever monoplane powered by various engines including the Continental C90-8, the Continental C90-14F and the Continental O-200-A, providing a top speed of 235 kmh.
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The Jurca MJ6 is a French two-seater low-wing cantilever monoplane designed for amateur construction. The Jurca MJ6 is designed to be powered by two Potez 4 E-20, Potez 4 E-30, Continantal C90-14F or Continental O-200-A four-cylinder horizontally-opposed air-cooled engines providing a top speed of 245 kmh and an endurance of three hours flying time.
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The Jurca MJ7 Gnatsum is a French, amateur-build, two-thirds scale replica of the Second World War North American P-51 Mustang fighter aircraft. The Jurca MJ7 Gnatsum is powered by a Walter Minor 6-III six-cylinder inverted in-line air-cooled engine providing a top speed of 260 kmh.
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The Jurca MJ8 1-Nine-O was a French single-seater amateur-build sporting aircraft consisting of a three-quarters scaled down model of the German Focke-Wulf Fw 190 fighter aircraft. The Jurca MJ8 was of wooden construction and powered by a any engine of between 100 and 200 hp, providing a top speed of about 260 kmh.
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Abbreviations
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