Hiro H2H
H2H1 on a launching trolly.
Role Patrol Flying boat
National origin Japan
Manufacturer Hiro Naval Arsenal
First flight 1930
Introduction 1932
Primary user Imperial Japanese Navy
Number built 17
Developed from Supermarine Southampton

The Hiro H2H, or "Navy Type 89 Flying boat" (Japanese: "八九式飛行艇"), was a Japanese patrol flying boat of the 1930s. Designed and built by the Hiro Naval Arsenal, it was a twin-engined biplane that was operated by the Imperial Japanese Navy.

Design and development

In 1929, the Imperial Japanese Navy purchased a single example of the British Supermarine Southampton II metal-hulled flying boat,[1] and after evaluation, it was passed onto the Hiro Naval Arsenal (who designed the wooden Hiro H1H flying boat based on the Felixstowe F.5), to study its advanced metal hull structure. Following this study, Hiro designed a new flying boat, closely resembling the Southampton.[2]

The new aircraft was a twin-engined biplane, with an all-metal hull, and fabric covered metal wing and tail structures. It was powered by two Hiro Type 14 water-cooled 12-cylinders W engines. The first prototype was completed in 1930, and following successful testing was ordered into production, with 13 aircraft being built by Hiro and a further four by Aichi. Later aircraft were powered by more powerful (600-750 hp (448-560 kW)) Hiro Type 90 engines.[3]

Operational history

It entered service in 1932 as the Type 89 Flying boat, with the short designation H2H1. Type 89 Flying Boats entered service in time for the Shanghai Incident, and along with Hiro's earlier H1H, served in front line service until the early years of the Second Sino-Japanese War.[4]

Specifications (Early version)

Data from Japanese Aircraft 1910-1941 [4]

General characteristics

  • Crew: 6
  • Length: 16.28 m (53 ft 5 in)
  • Wingspan: 22.14 m (72 ft 8 in)
  • Height: 6.13 m (20 ft 1 in)
  • Wing area: 120.5 m2 (1,297 sq ft)
  • Empty weight: 4,368 kg (9,630 lb)
  • Gross weight: 6,500 kg (14,330 lb)
  • Powerplant: 2 × Hiro Type 14 12-cylinder water-cooled W engine, 410 kW (550 hp) each
  • Propellers: 4-bladed wooden propellers

Performance

  • Maximum speed: 191.9 km/h (119.2 mph, 103.6 kn)
  • Cruise speed: 130 km/h (81 mph, 70 kn) at 1,000 m (3,300 ft)
  • Endurance: 14.5 hr
  • Service ceiling: 4,320 m (14,170 ft)
  • Time to altitude: 19 min to 3,000 m (9,800 ft)

Armament

  • Guns: 4× 7.7 mm machine guns (two in bow, one each in port and starboard mid-ships stations)
  • Bombs: Two 250 kg (550 lb) bombs

See also

Related development

Aircraft of comparable role, configuration, and era

Related lists

References

Notes

  1. ↑ Andrews and Morgan 1987, p.110.
  2. ↑ Mikesh and Abe 1990, pp. 95-96.
  3. ↑ Mikesh and Abe 1990, pp.96-97.
  4. 1 2 Mikesh and Abe 1990, p.97.

Bibliography

  • Andrews, C.F. and Morgan, E.B. Supermarine Aircraft since 1914. London:Putnam, 1987. ISBN 0-85177-800-3.
  • Mikesh, Robert C. and Abe, Shorzoe. Japanese Aircraft 1910-1941. London:Putnam, 1990. ISBN 0-85177-840-2.
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