Aichi AB-6
| AB-6 | |
|---|---|
| Role | Reconnaissance floatplane |
| National origin | Japan |
| Manufacturer | Aichi |
| Designer | Tetsuo Miki |
| First flight | 1933 |
| Number built | 1 |
| Developed from | Heinkel He 62 |
The Aichi AB-6, or Aichi Experimental 7-Shi Reconnaissance Seaplane, was a prototype Japanese reconnaissance floatplane. It was a single-engined, three-seat biplane intended for the Imperial Japanese Navy, but only one was built, the rival aircraft from Kawanishi, the E7K being preferred.
Design and development
[edit]In 1932, the Imperial Japanese Navy raised a specification for a long-range floatplane reconnaissance aircraft to replace its Yokosuka E1Y and E5Y operating from its seaplane tenders and battleships, requesting prototypes from Aichi and Kawanishi. Aichi's entry, the Aichi AB-6 or Aichi Experimental 7-Shi Reconnaissance Seaplane,[a] designed by Tetsuo Miki, was based on the Heinkel He 62, one example of which had been imported by Aichi the previous year for evaluation against a similar requirement. The AB-6 was a biplane with folding wings for storage aboard ship, of all-metal construction with fabric covering, and powered by a single Hiro Type 91 W12 engine. Its crew of three, pilot, observer and radio operator/gunner were accommodated in an enclosed cockpit.[1]
Operational history
[edit]The prototype was completed in February 1933 and made its maiden flight from Nagoya harbor. While it had good handling in the air, its speed, take-off, and landing performance was disappointing, and the aircraft was modified to try to improve matters. It was fitted with revised wings, of different aerofoil section and with full-span leading edge slats. The original Hamilton-Standard two-bladed metal variable-pitch propeller was first replaced by a two-bladed wooden propeller and then a four-bladed wooden unit. Despite these changes, Kawanishi's design remained superior, and in 1934, was ordered into production as the Navy Type 94 Reconnaissance Seaplane, or Kawanishi E7K.[2][3]
Specifications (final configuration)
[edit]Data from Japanese Aircraft 1910–1941[4]
General characteristics
- Crew: 3
- Length: 10.44 m (34 ft 3 in)
- Wingspan: 12.98 m (42 ft 7 in)
- Height: 4.80 m (15 ft 9 in)
- Wing area: 40.61 m2 (437.1 sq ft)
- Empty weight: 1,920 kg (4,233 lb)
- Gross weight: 3,020 kg (6,658 lb)
- Max takeoff weight: 3,300 kg (7,275 lb)
- Powerplant: 1 × Hiro Type 91 water-cooled W12 engine, 470 kW (630 hp)
Performance
- Maximum speed: 230 km/h (140 mph, 120 kn) at sea level
- Cruise speed: 150 km/h (92 mph, 80 kn) at 1,000 m (3,300 ft)
- Stall speed: 81 km/h (50 mph, 44 kn)
- Endurance: 11.9 h
- Service ceiling: 4,850 m (15,910 ft)
- Time to altitude: 3,000 m (9,840 ft) in 14 min 54 s
Armament
- Guns: 1× fixed, forward firing 7.7 mm machine gun, 1 flexibly mounted in rear cockpit and 1× under fuselage
See also
[edit]Aircraft of comparable role, configuration, and era
Notes
[edit]- a In the Japanese Navy designation system, specifications were given a Shi number based on the year of the Emperor's reign it was issued. In this case 7-Shi stood for 1932, the 7th year of the Shōwa era.[5]
References
[edit]- Francillon, R.J. Japanese Aircraft of the Pacific War. London:Putnam, 1970. ISBN 0-370-00033-1.
- Mikesh, Robert and Shorzoe Abe. Japanese Aircraft 1910–1941. London:Putnam, 1990. ISBN 0-85177-840-2.