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Kyushu J7W1 Shinden

Kyushu J7W1 Shinden

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2540000 가격
400 생존력
5015 kg중량
507.1 공격력
1547.4 비행 속력
720 km/h해수면 최고 속도
720 km/h최적 고도 최고 속력
1400 m최적 고도
800 km/h최고 강하 속도
118.4 m/s상승 속력
120 km/h실속 속도
387 km/h최적 비행 속력
85.4 조작성
10.8 초평균 360도 회전 속도
100 °/s횡전율
1244.8 기동성
Kyushu J7W1 Shinden
일본 열도에 가해지던 미국의 폭격에 대항할 목적으로 설계된 요격기이다. 전쟁이 끝나기 전 완성된 단 2기의 시제기는 미군이 포획하였다.



단계 엔진 엔진 출력, hp / 추력 유형 중량, kg 가격,
IX NAME_MODULE_MK10B_SPEC_TOP_J7W1_1 3100 공랭식 1520 179000
IX MK9F 2500 공랭식 1240 162000
IX MK10B 3100 공랭식 1520 179000


단계 기체 생존력 중량, kg 가격,
VIII J7W1 400 3575 140000
엔진 덮개 장착 무기

엔진 덮개 장착 무기

단계 기관총 구경 포구 속도, m/s 공격력 연사력, 발/분 중량, kg 가격,
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
외부 장착 무장

외부 장착 무장

단계 폭탄 피해 반경, m 공격력 중량, kg 가격,
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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Japan INakajima Type-91 VIIMitsubishi J4M Senden VIIIKyushu J7W1 Shinden IXKyushu J7W2 Shinden-Kai XKyushu J7W3