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Kyushu J7W1 Shinden

Kyushu J7W1 Shinden

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J7W1

Icon
Totals
2540000 Kosten
400 Überlebensfähigkeit
5015 kgGewicht
507.1 Schaden
Speed
1547.4 Fluggeschwindigkeit
720 km/hV(max.) auf Meeresspiegel
720 km/hV(max.) bei opt. Flughöhe
1400 mOptimale Höhe
800 km/hMax. Sturzfluggeschw.
118.4 m/Sek.Steigrate
120 km/hGeschwindigkeit Strömungsabriss
387 km/hOptimale Fluggeschwindigkeit
Mobility
85.4 Steuerbarkeit
10.8 Sek.Mittlere Zeit für 360-Grad-Kurve
100 °/Sek.Rollrate
1244.8 Manövrierbarkeit
VIII
Kyushu J7W1 Shinden
2540000
Abfangjäger, der den US-amerikanischen Bomberangriffen auf die japanischen Inseln entgegnen sollte. Zwei Prototypen wurden bis Ende des Kriegs fertig gestellt.

Motor

Motor

Stufe Motor Motorleistung, PS / Schub Typ Gewicht, kg Kosten,
IX NAME_MODULE_MK10B_SPEC_TOP_J7W1_1 3100 luftgekühlt 1520 179000
IX MK9F 2500 luftgekühlt 1240 162000
IX MK10B 3100 luftgekühlt 1520 179000
Flugwerk

Flugwerk

Stufe Flugwerk Überlebensfähigkeit Gewicht, kg Kosten,
VIII J7W1 400 3575 140000
Haubenmontierte Waffe

Haubenmontierte Waffe

Stufe Maschinengewehr Kaliber Mündungsgeschwindigkeit, m/Sek. Schaden Feuerrate, Schuss/Min. Gewicht, kg Kosten,
VII 20 mm Type 99-2 Model 5 (H) 20 1600 110 400 90 60900
IX 30 mm Type 5 (H) 30 1040 220 170 120 80500
IX WEAPON_NAME_G30MM-TYPE5-F_SPEC_TOP_J7W1_1 30 1040 220 170 120 80500
Außenwaffe

Außenwaffe

Stufe Bomben Schadensradius, m Schaden Gewicht, kg Kosten,
VI 250 kg 75 4400 250 1200


Compatible Equipment

Compatible Consumables


Historical Info

The "J-" designation of J7W1 referred to land-based fighters of the IJN and the "-W-" to Watanabe Tekkōjo, the company that oversaw the initial design; Watanabe changed its name in 1943 to Kyūshū Hikōki K.K.


The idea of a canard-based design originated with Lieutenant Commander Masayoshi Tsuruno, of the technical staff of the IJN in early 1943. Tsuruno believed the design could easily be retrofitted with a turbojet, when suitable engines became available. His ideas were worked out by the First Naval Air Technical Arsenal (Dai-Ichi Kaigun Koku Gijitsusho), which designed three gliders designated Yokosuka MXY6, featuring canards. These were built by Chigasaki Seizo K. K. and one was later fitted with a 22 hp Semi 11 (Ha-90) 4-cylinder air-cooled engine.

The feasibility of the canard design was proven by both the powered and unpowered versions of the MXY6 by the end of 1943, and the Navy were so impressed by the flight testing, they instructed the Kyushu Aircraft Company to design a canard interceptor around Tsuruno's concept. Kyushu was chosen because both its design team and production facilities were relatively unburdened, and Tsuruno was chosen to lead a team from the First Naval Air Technical Arsenal to aid Kyushu's design works.

The construction of the first two prototypes started in earnest by June 1944, stress calculations were finished by January 1945, and the first prototype was completed in April 1945. The 2,130 hp Mitsubishi MK9D (Ha-43) radial engine and its supercharger were installed behind the cockpit and drove a six-bladed propeller via an extension shaft. Engine cooling was to be provided by long, narrow, obliquely mounted intakes on the side of the fuselage. It was this configuration that caused cooling problems while running the engine while it was still on the ground. This, together with the unavailability of some equipment parts postponed the first flight of the Shinden.

Even before the first prototype took to the air the Navy had already ordered the J7W1 into production, with quotas of 30 Shinden a month given to Kyushu's Zasshonokuma factory and 120 from Nakajima's Handa plant. It was estimated some 1,086 Shinden could be produced between April 1946 and March 1947.

On 3 August 1945, the prototype first took off, with Tsuruno at the controls, from Itazuke Air Base.[4][10] Two more short flights were made, a total of 45 minutes airborne, by war's end. Flights were successful, but showed a marked torque pull to starboard (due to the powerful engine), some flutter of the propeller blades, and vibration in the extended drive shaft.

The production of J7W was canceled due to the end of World War II. The type never saw combat.



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UK IGloster Goldfinch IIHawker Demon IIIBlackburn Skua IVHawker Hurricane Mk I VHawker Hurricane Mk II VHawker Hurricane IID VIHawker Tornado VIIHawker Typhoon VIIISupermarine Seafang F.32 VIIIHawker Tempest IXHawker Sea Hawk XHawker Hunter
Germany IArado Ar 65 IVArado Ar 197 VFocke-Wulf Fw 190 A-1 VIFocke-Wulf Fw 190 A-5 VIIFocke-Wulf Fw 190 A-8/R2 VIIFocke-Wulf Fw 190 D VIIIMesserschmitt Me 109 TL VIIIBlohm und Voss P.210 IXBlohm und Voss P.212.03 XBlohm und Voss P.215.02
USSR IPolikarpow I-5 IIPolikarpow I-15 IIPolikarpow I-5 ShKAS IIIKotscherigin-Jazenko DI-6i IIIPolikarpow I-16 (frühe Ausf.) IVPolikarpow I-16 (späte Ausf.) IVPolikarpow I-16 Typ 29 IVBorowkow-Florow I-207/4 IVLawotschkin LaGG-3 Serie 4 VLawotschkin LaGG-3 Serie 34 VCurtiss P-40 M-105 VJakowlew Jak-7 VJakovlev Jak-7 M-82 VIIljuschin IL-1 VIJakowlew Jak-9 VIIJakowlew Jak-9U VIIIMikojan-Gurewitsch I-260 VIIISuchoi Su-9 IXAlexejew I-211 XAlexejew I-215
China IICurtiss Hawk III
Japan INakajima Type-91 VIIMitsubishi J4M Senden VIIIKyushu J7W1 Shinden IXKyushu J7W2 Shinden-Kai XKyushu J7W3