Kawasaki KAT-1
Tampilan
![](http://upload.wikimedia.org/wikipedia/commons/thumb/e/e7/Kawasaki_KAT-1.png/220px-Kawasaki_KAT-1.png)
Kawasaki KAT-1 adalah pesawat pelatih milik Jepang dengan kursi dua. Pesawat ini dirancang untuk bersaing dalam sayembara kontrak desain pesawat bagi Angkatan Pertahanan Udara Jepang di pertengahan 1950-an. Hanya dua buah saja yang diselesaikan.
Spesifikasi
[sunting | sunting sumber]Data from Jane's All the World's Aircraft 1956/57[1]
General characteristics
- Crew: Dua
- Length: 850 m (2.788 ft 9 in)
- Wingspan: 1.150 m (3.773 ft 0 in)
- Height: 280 m (918 ft 8 in)
- Wing area: 186 m2 (2.000 sq ft)
- Aspect ratio: 7.1
- Airfoil: NACA 2R1 16.5 di ekor, NACA 2410 di moncong
- Empty weight: 1.070 kg (2.359 pon)
- Gross weight: 1.385 kg (3.053 pon)
- Powerplant: 1 × Lycoming GO-435-C2B 6-silinder horizontally opposed air-cooled, 180 kW (240 hp)
- Propellers: 2-bladed Hartzell Propeller, 2,29 m (7 ft 6 in) diameter metal, variable pitch
Performance
- Maximum speed: 303 km/h (188 mph; 164 kn) at sea level
- Cruising speed: 225 km/h (140 mph; 121 kn) 40% power pada 2,135 m (7,000 ft)
- Range: 1.140 km (708 mi; 616 nmi) maximum, at 40% power pada 3,050 m (10,000 ft)
- Service ceiling: 6.100 m (20.013 ft) service
- Rate of climb: 56 m/s ([convert: unit mismatch]) initial
- Wing loading: 745 kg/m2 (153 pon/sq ft)
- Power/mass: 129 W/kg (0.079 hp/lb)
- Take-off run: 168 m (550 ft) at sea level, no wind
- Landing run: 206 m (680 ft) at sea level, no wind
- Landing speed: 83.5 km/h (52 mph) with flaps extended
Referensi
[sunting | sunting sumber]- ^ Kesalahan pengutipan: Tag
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tidak sah; tidak ditemukan teks untuk ref bernamaJAWA56
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