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Prototype single-seat assault aircraft
The prototype single-seat surprise attack aircraft (Shisakutanzaki Shuki) is
an attack aircraft jointly planned by the Imperial Japanese Army and the
Imperial Japanese Navy. There is no plan number or abbreviated code
because it is a site planning machine.
overview
In April 1945, Singaporean army and navy officials announced the
"Southern Self-Support Plan," a local production plan for a special attack
aircraft using a spare 1,000-horsepower-class air-cooled
engine and propeller, which had been used for about 250 aircraft. Planned
by The design was carried out from the beginning of May 1945, led by Shinroku Inoue, an engineer of the Tokyo Air Service, who was dispatched to the 3rd Air Force Headquarters as an Army administrator. cooperated with it. Production
of the aircraft began in June 1945, but development halted at the end of
World War II, and several sets of fuselages and wings that had been assembled
at the end of the war were scrapped.
The fuselage is made of wood, except for the fuselage framework that uses
steel pipes. Locally procured engines were used, and various equipment such
as fixed legs were used from the damaged aircraft. It was also designed for dive bombing at a descent angle of 60 degrees.
Specifications
Total length: 8.35m
Width: 11.35 m
Main wing area: 20.0 m2
Weight: 2,500 kg
Takeoff weight: 3,000 kg
Engine: Locally procured air-cooled (1,000 hp class) x 1
Armament: 250kg bomb x 1
Crew: 1 person
profilbaru-com.translate.goog
Prototype single-seat assault aircraft
The prototype single-seat surprise attack aircraft (Shisakutanzaki Shuki) is
an attack aircraft jointly planned by the Imperial Japanese Army and the
Imperial Japanese Navy. There is no plan number or abbreviated code
because it is a site planning machine.
overview
In April 1945, Singaporean army and navy officials announced the
"Southern Self-Support Plan," a local production plan for a special attack
aircraft using a spare 1,000-horsepower-class air-cooled
engine and propeller, which had been used for about 250 aircraft. Planned
by The design was carried out from the beginning of May 1945, led by Shinroku Inoue, an engineer of the Tokyo Air Service, who was dispatched to the 3rd Air Force Headquarters as an Army administrator. cooperated with it. Production
of the aircraft began in June 1945, but development halted at the end of
World War II, and several sets of fuselages and wings that had been assembled
at the end of the war were scrapped.
The fuselage is made of wood, except for the fuselage framework that uses
steel pipes. Locally procured engines were used, and various equipment such
as fixed legs were used from the damaged aircraft. It was also designed for dive bombing at a descent angle of 60 degrees.
Specifications
Total length: 8.35m
Width: 11.35 m
Main wing area: 20.0 m2
Weight: 2,500 kg
Takeoff weight: 3,000 kg
Engine: Locally procured air-cooled (1,000 hp class) x 1
Armament: 250kg bomb x 1
Crew: 1 person
試作単座奇襲機
試作単座奇襲機（しさくたんざきしゅうき）は、大日本帝国陸軍と大日本帝国海軍が共同計画した攻撃機。現地計画機のため計画番号や略符号は存在しない。 概要...
