Kawasaki Ki-102

Airplanes

Length

11.45 m

Flat Wing Span

15.57 m

Height

3.7 m

Flat Wing Area

34 m²

Max Speed

580 km/h

Max Ceiling

10000 m

Number of Engines

First Flight

1944-01-01

Entry Into service

1944-01-01

Number Built

238

Maximum Range

2000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Range (km)
Kawasaki Ki-102	2000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Kawasaki Ki-96		11.45	15.57		Compare
Dornier Do 28	Lycoming O-540	11.41	15.55	12	Compare
Grigorovich MR-5		11.4	15.6		Compare
Praga E-51		11.69	15.6		Compare
Dayton-Wright FP.2	Liberty L-6	11.23	15.67	3	Compare
Polikarpov TIS	Mikulin AM-37	11.7	15.5		Compare

All data (24 fields)

Name: Kawasaki Ki-102
Manufacturer: Kawasaki Heavy Industries
Description: The Kawasaki Ki-102 or was a twin-engine, two-seat, long-range heavy fighter developed to replace the Ki-45 Toryū.
First Flight: 1944-01-01
Entry Into service: 1944-01-01
Service End: 1945-01-01
Designer: Kawasaki Heavy Industries
Type: Attacker, fighter, night fighter
Length (m): 11.45
Height (m): 3.7
Cockpit Crew: 2
Max Speed (km/h): 580
Max Ceiling (m): 10000
Rate of Climb (m/s): 11.9
Armament: ; 1 × 57 mm (2.24 in) Ho-401 cannon—replaced in the 102a with a 37 mm (1.46 in) Ho-204 cannon, deleted in the 102 C; 2 × 20 mm Ho-5 cannon in the belly—replaced in the 102 C with 30 mm (1.18 in) cannon in the package, plus oblique-firing 2 × 20 mm cannon; 1 × 12.7 mm (0.50 in) Ho-103 machine gun (deleted in the Ki-102a and Ki-102); ; 2 × 200 L (53 US gal) drop tanks; or; 2 × 250 kg (551 lb) bombs…
National Origin: Japan
Number Built: 238
Powerplant Description: 2 × Mitsubishi Ha112-II Ru 14-cylinder air-cooled radial engine, 1120 kW (1502 hp) each
Primary Users: Imperial Japanese Army Air Force
Status: Retired
Wikipedia Article (URL): en.wikipedia.org/wiki/Kawasaki_Ki-102
Flat Wing Span (m): 15.57
Flat Wing Area (m²): 34
Number of Engines: 2