Nakajima Ki-43-II Hayabusa
GENERAL DATA |
Hayabusa
= Peregrine Falcon, Army Type 1 Fighter, Oscar (Allied reporting
name) |
Fighter,
Fighter bomber
|
1 |
Nakajima Hikoki
K.K. at Ota, Tachikawa Hikoki K.K. at Tachikawa, 1st Army Air Arsenal |
Ki-43-II prototype:
5, Ki-43-II service trials: 3, Ki-43-II
/ Ki-43-III: 5190
November 1942 - October 1944 (Nakajima), May 1943 - August 1945
(Tachikawa) |
Early January 1939 (prototype) |
October 1941 (Ki-43-I) |
Variants |
Had a two speed super charged Ha-115 engine
(1,150 HP). There was a constant speed three bladed propeller. |
Mostly used as a fighter bomber. |
Army Type 1 Fighter Model 2A: The wing
was "clipped". Windscreen and canopy were altered. 13 mm
armor protection for the pilot was added. Crude self sealing fuel
tanks were installed. Hard points under wings. |
Army Type 1 Fighter Model 2B: Had
2: 12.7 mm machine guns in wings. Hard points in wings were repositioned.
|
To make production easier airframe modifications were
made. |
DIMENSIONS |
1910 kg |
2590 kg |
2925 kg |
8.92 m |
3.27 m |
10.84 m |
21.4 m² |
121 kg/m² |
ARMAMENT (Ki-43-IIb) |
2× 12.7 mm (.50 in) Ho-103 |
2 x 270 |
2× 12.7 mm (.50 in) Ho-103 |
2 x 270 |
- |
- |
2 x 250 kg bomb |
(*) 2 × fixed, forward-firing in the cowl
Armament variations:
Ki-43-II-Ko & Ki-43-IIa:
2× 12.7 mm (0.50 in) Ho-103 MG (nose) only
POWERPLANT |
1 ×
Nakajima Ha-115 |
14-cylinder air-cooled
radial, 27.9 L |
1150hp
|
444 hp / ton * |
564 l (internal),
2x 170 l (external)
|
(*) with Loaded Weight
PERFORMANCES |
536 km/h
at 6000 m |
355 km/h at 4000 m |
? km/h |
11200 m |
20 m/s |
1760 km, 3200 km (ferry range) |
(*) vitesse de décrochage
|