Kawasaki Ki-100 “Goshikisen”
The Kawasaki Ki-100 "Goshikisen" is a single-seat, single-engine monoplane fighter aircraft used by the Imperial Japanese Army Air Service.
Kawasaki Ki-100 "Goshikisen"- Japanese WW2 Aircraft

Kawasaki Ki-100 Aircraft Overview

The Kawasaki Ki-61 was a single-engine fighter aircraft developed by the Japanese company Kawasaki Heavy Industries during World War II. The aircraft was also known by its Allied reporting name “Tony”.

The Ki-61 was designed to meet the Japanese army’s requirements for a high-performance fighter to replace the earlier Ki-43 Hayabusa. The first prototype flew in December 1941, and the Ki-61 entered service with the Japanese army in 1943.

The Ki-61 was a low-wing monoplane with a liquid-cooled inline engine and retractable landing gear. It was armed with two 20mm cannon and two 7.7mm machine guns mounted in the wings. Later variants of the Ki-61 were equipped with additional guns and rockets for ground attack missions.

The Ki-61 was considered one of the best Japanese fighters of the war, with excellent performance and maneuverability. It saw combat in the Pacific, China, and Southeast Asia, and was used by some of Japan’s top fighter aces. However, it was also plagued by engine reliability problems and suffered from a lack of spare parts due to Japan’s dwindling industrial resources.

Despite these issues, the Ki-61 remained in service until the end of the war, and was used in several major campaigns, including the defense of the Philippines and the defense of Japan. It was also exported to other countries, including Thailand and Manchukuo.

Kawasaki Ki-100-I-Ko Specifications

  • Crew: One
  • Length: 8.82 m (28 ft 11 in)
  • Wingspan: 12.00 m (39 ft 4 in)
  • Height: 3.75 m (12 ft 4 in)
  • Wing area: 20 m2 (220 sq ft)
  • Airfoil: NACA 2R1 16 (root), NACA 24009 (tip)
  • Empty weight: 2,525 kg (5,567 lb)
  • Gross weight: 3,495 kg (7,705 lb)
  • Fuel capacity: 595 L (157 US gal; 131 imp gal) (internal fuel)
  • Water methanol capacity: 95 L (21 imp gal; 25 US gal)
  • Undercarriage track: 4.050 m (13.29 ft)
  • Powerplant: 1 × Mitsubishi Ha-112-II/Ha-33 14-cylinder two row air-cooled radial engine, 1,120 kW (1,500 hp) at take off
  • Propellers: 3-bladed constant-speed propeller, 3.00 m (9 ft 10 in) diameter

Kawasaki Ki-100-I-Ko Performance

  • Maximum speed: 580 km/h (360 mph, 310 kn) at 6,000 m (20,000 ft)
  • Cruise speed: 400 km/h (250 mph, 220 kn) at 4,000 m (13,000 ft)
  • Range: 1,400 km (870 mi, 760 nmi) on internal fuel only, 2,200 km (1,400 mi; 1,200 nmi) with 2 x 200 L (44 imp gal; 53 US gal) external droppable fuel tanks
  • Endurance: 3 hours 30 minutes
  • Service ceiling: 11,000 m (36,000 ft)
  • Time to altitude: ** 6 minutes to 5,000 m (16,000 ft)
    • 20 minutes to 10,000 m (33,000 ft)
  • Wing loading: 174.8 kg/m2 (35.8 lb/sq ft)

Kawasaki Ki-100-I-Ko Armament

  • Guns: 2 × 20 mm (0.8 in) fuselage-mounted Ho-5 cannons and 2 × 12.7 mm (0.50 in) wing-mounted Ho-103 machine guns
  • Hardpoints: 2 × 200 L (44 imp gal; 53 US gal) external drop tanks, carried outboard of the undercarriage legs
  • Bombs: 2 × 250 kg (550 lb) bombs, carried in lieu of drop tanks on same hardpoints outboard of the undercarriage.

Kawasaki Ki-100 Image Gallery

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