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Kyushu J7W1 Shinden

Kyushu J7W1 Shinden

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J7W1

Icon
Totals
2540000 Prix
400 Capacité de survie
5015 kgPoids
507.1 Dégâts
Speed
1547.4 Vitesse
720 km/hVitesse max. au ras du sol
720 km/hVitesse max. à altitude idéale
1400 mAltitude optimale
800 km/hVitesse en piqué
118.4 m/sTaux de montée
120 km/hVitesse de décrochage
387 km/hVitesse optimale
Mobility
85.4 Contrôlabilité
10.8 sTemps moyen de rotation 360°
100 °/sTaux de roulis
1244.8 Maniabilité
VIII
Kyushu J7W1 Shinden
2540000
Intercepteur conçu pour contrer les raids de bombardements américains sur les îles Japonaises. Seuls deux prototypes furent construits avant la fin de la guerre.

Moteur

Moteur

Rang Moteur Puissance du moteur, ch / Poussée Type Poids, kg Prix,
IX NAME_MODULE_MK10B_SPEC_TOP_J7W1_1 3100 refroidi à l'air 1520 179000
IX MK9F 2500 refroidi à l'air 1240 162000
IX MK10B 3100 refroidi à l'air 1520 179000
Cellule d'avion

Cellule d'avion

Rang Cellule d'avion Capacité de survie Poids, kg Prix,
VIII J7W1 400 3575 140000
Armement du carénage

Armement du carénage

Rang Mitrailleuse Calibre Vitesse initiale, m/s Dégâts Cadence de tir, coups/min Poids, kg Prix,
VII 20 mm Type 99-2 Model 5 (C) 20 1600 110 400 90 60900
IX 30 mm Type 5 (C) 30 1040 220 170 120 80500
IX WEAPON_NAME_G30MM-TYPE5-F_SPEC_TOP_J7W1_1 30 1040 220 170 120 80500
Armement extérieur

Armement extérieur

Rang Bombes Rayon des dégâts, m Dégâts Poids, kg Prix,
VI 250 kg 75 4400 250 1200


Compatible Equipment

Compatible Consumables


Informations Historiques

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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USSR IPolikarpov I-5 IIPolikarpov I-15 IIPolikarpov I-5 ShKAS IIIKotcherigine-Yatsenko DI-6i IIIPolikarpov I-16 (mod. initial) IVPolikarpov I-16 (mod. tardif) IVPolikarpov I-16 Type 29 IVBorovkov-Florov I-207/4 IVLavotchkine LaGG-3 série 4 VLavotchkine LaGG-3 série 34 VCurtiss P-40 M-105 VYakovlev Yak-7 VYakovlev Yak-7 M-82 VIIliouchine IL-1 VIYakovlev Yak-9 VIIYakovlev Yak-9U VIIIMikoyan-Gourevitch I-260 VIIISukhoi Su-9 IXAlekseyev I-211 XAlekseyev I-215
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Japan INakajima Type-91 VIIMitsubishi J4M Senden VIIIKyushu J7W1 Shinden IXKyushu J7W2 Shinden-Kai XKyushu J7W3