Nakajima J5N
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| Nakajima J5N | |
|---|---|
 Nakajima J5N1 Tenrai |
|
| Type | |
| Manufacturer | Nakajima |
| Designed by | Katsuji Nakamura, Kazuo Ohno |
| Maiden flight | July, 1944 |
| Primary user | Imperial Japanese Navy |
| Number built | 6 |
During the spring of 1943, the JNAF issued an 18-Shi specification for a single-seat twin-engine interceptor capable of reaching a top speed of 414 mph at 19,685 ft. Nakajima submitted a proposal based on the earlier J1N1 Gekko three-seat night fighter, although this new aircraft – designated J5N1 – was slightly smaller. The layout of the J5N was similar to the J1N, a low set wing on which were mounted the two engines, these being 1,990 hp Nakajima Homare 21 eighteen-cylinder air-cooled radials, with a long fuselage ending in a conventional tail arrangement. For maximum utilization of the power from the twin engines, large four-blade propellers were fitted, and these also featured large spinners – as fitted to the J1N. The main wheels retracted rearwards into the engine nacelles, and the tail wheel was fixed. The cockpit was set above the wing, and featured a starboard opening canopy. The nose was streamlined to offer the pilot an excellent forward view during landing, take-off and taxiing.
The armament of the J5N was impressive, and consisted of two 30mm and two 20mm cannon, and provision was made for a centreline 500 lb bomb. The J5N was designed to combat the heavily armed US fighters in the Pacific Theatre at that time, and, thus, the armament would have done severe damage to these aircraft. To concentrate the firepower, the four cannons were mounted in the nose of the J5N.
Impressed with the design, the JNAF authorized the development of the J5N1, assigned the name Tenrai (Heavenly Thunder), and six prototypes were requested to be built. The first prototype – lacking its armament – made its first flight July 13, 1945, and was something of a disappointment. The top speed attained was only 371 mph – far below the specified 414 mph of the requirement. Despite the other five prototypes flying as well, with numerous enhancements, the aircraft never achieved its design speed, and the project was abandoned soon after.
[edit] Variants
- J5N1 : Single-seat interceptor fighter aircraft. Six built.
[edit] Specifications (J5N1)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.General characteristics
- Crew: one, pilot
- Length: 11.46 m (37 ft 7 in)
- Wingspan: 14.00 m (45 ft 11 in)
- Height: 2.38 m (7 ft 9 in)
- Wing area: 32 m² (344 ft²)
- Empty weight: 5,195 kg (11,429 lb)
- Loaded weight: 7,350 kg (16,170 lb)
- Powerplant: 2× Nakajima Homare 21 18-cylinder radial engines, 1,485 kW (1,990 hp) each
Performance
- Maximum speed: 619 km/h (387 mph)
- Rate of climb: 900 m/min (2,950 ft/min)
- Wing loading: 230 kg/m² (47 lb/ft²)
- Power/mass: 0.40 kW/kg (0.24 hp/lb)
Armament
- 2 × 30 mm cannon and/or 2x 20 mm Type 99-2 cannon
- 1 × 250 kg (550 lb) bomb
[edit] References
[edit] Notes
[edit] Bibliography
- Francillon, Réne J. Japanese Aircraft of the Pacific War. London: Putnam & Company Ltd., 1970 (2nd edition 1979). ISBN 0-370-30251-6.
- Green, William. Warplanes of the Second World War, Volume Three: Fighters. London: Macdonald & Co.(Publishers) Ltd., 1961. ISBN 0-356-1447-9.
- Townend, David R. Thunderbolt & Lightning. Markham: AeroFile Publications, 2008, ISBN 978-0-9732020-2-1.
[edit] See also
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