Mitsubishi A5M 'Claude'

Moderators: Messalina, Tandorini

Mitsubishi A5M 'Claude'

Berichtdoor Tandorini » 18 apr 2009, 08:34

Afbeelding

Afbeelding

Verkleinde Afbeelding
Verkleinde afbeelding. Klik om te vergroten.

In February 1934 the Imperial Japanese Navy drew up its specification for a new single-seat fighter, the requirements including a challenging maximum speed of 217 mph (350 km/h) and a rate of climb that would take it to 16,405 ft (5000 m) in only 6 minutes 30 seconds. Mitsubishi took up this challenge with a design team headed by Jiro Horikoshi, later to gain his place in aviation history for the remarkable A6M Zero, working against difficult odds to gain what was seen by Mitsubishi to be a potentially important contract. All single-seat fighters then in service with the navy were of biplane configuration so the team's monoplane layout was seen as something of a gamble, especially as an earlier monoplane design from Mitsubishi had failed to gain the navy's approval. Horikoshi's design for the prototype united an inverted gull wing to a narrow section fuselage, the gull wing being chosen to cornbine a large-diameter propeller with main landing gear units that would be as short as possible. The tail unit was conventional, the powerplant was a 550-hp (410kW) Nakajima Kotobuki (congratulation) 5 radial engine, and the pilot was accommodated in an open cockpit directly over the wing. Designated Mitsubishi Ka-14, it was flown for the first time on 4 February 1935 and demonstrated very quickly that it was more than capable of meeting the navy's requirements. In early tests a maximum speed of 280 mph (450 km/h) was recorded, and the climb to 16,405 ft (5000 m) was achieved in only 5 minutes 54 seconds. There were, however, aerodynamic shortcomings and so the second prototype was given a conventional cantilever low wing with split trailing-edge flaps; at the same time a 560-hp (418-kW) Kotobuki 3 engine was installed. Four other prototypes were completed with varying powerplants, and it was with the low-wing configuration of the second prototype combined with a 585-hp (436kW) Kotobuki 2 KAI-1 engine that the Mitsubishi A5M1 was ordered into production as the Navy Type 96 Carrier Fighter Model.

The A5M1 of 1936 was the Japanese navy's first monoplane fighter, the basic model being armed with two forward-firing 7.7-mm (0.303-in) machine-guns, but the A5M1a variant carried two 20-mm Oerlikon FF cannon. The A5M2 of 1937 was regarded as the most important fighter aircraft in the navy's inventory during the 8ino-Japanese War, the performance of the initial A5M2a being improved, by comparison with the A5M1, by installation of the 610-hp (455-kW) Kotobuki 2-KAI-3 engine; the ensuing generally similar A5M2b differed primarily by the introduction of more power, in the shape of the 640-hp (477-kW) Kotobuki 3, and early production aircraft had an enclosed cockpit. This did not prove popular with its pilots, and late-production A5M2b fighters reverted to open cockpit configuration. Under the designation A5M3 two experimental aircraft were built and these, similar to earlier open-cockpit production aircraft, each had a 61O-hp (455-kW) Hispano Suiza 12Xcrs 'moteur canon' engine installed, with a 20-mm cannon firing through the propeller hub. Final production version was the A5M4 with the uprated Kotobuki 41 radial engine, and under the designation A5M4-K a total of 103 was completed as tandem two-seat trainers. At the outbreak of war in the Pacific the A5M4 was then the navy's standard fighter, but this situation was of only short duration for, when confronted by Allied fighter aircraft, the A5M's performance was soon found to be inadequate; by the summer of 1942 the type had been relegated to second-line duties.

The A5M had also come very close to being procured by the Japanese army, for the remarkable performance of the second prototype had resulted in a similar prototype being evaluated by the army under the designation Ki-18. Flown in competitive evaluation against the Kawasaki Ki-10-I biplane then entering service it was found to be considerably faster but inferior in manoeuvrability. Two modified and reengined Ki-18s were submitted for further testing under the designation Ki-33, but still lacking in manoeuvrability failed to gain an army contract. Production of all versions of the A5M, which was allocated the Allied codename 'Claude', reached a total of 1,094, built by Mitsubishi (791), the Omura Naval Air Arsenal (264) and Watanabe (39). In the final stages of the Pacific war A5M4s and A5M4-Ks were used in a kamikaze role against Allied shipping operating off Japan's coastal waters.
Versions

Ka-14

Six prototypes with various engines and design modifications.

A5M1

Navy carrier-based fighter, Model 1: first production model with 850 hp Kotobuki 2 KAI I engine.

A5M2/2a

Model 21: More powerful engine.

A5M2b

Model 22: First production examples with NACA cowling and 640 hp Kotobuki 3 engine.

A5M3a

Prototypes with 601 hp Hispano-Suiza 12 Xcrs engine.

A5M4

Model 24 (ex-Model 4): The A5M2b with different engine, closed cockpit, additional detachable fuel tank. The last production models (Model 34) with Kotobuki 41 KAI engine.

A5M1-A5M4

780 constructed by Mitsubishi. 39 constructed by Watanabe, 161 manufactured by Naval Ohmura Arsenal.

A5M4-K

Two seat trainer version of A5M4, 103 constructed by Naval Ohmura Arsenal.

Ki-18

Single prototype land-based version for IJAAF, based on the A5M. 550 hp Kotobuki 5 engine.

Ki-33

Two prototypes, a development of Ki-18 with a different engine, and closed cockpit.

Total Production (all versions): 1,094

Specifications (Mitsubishi A5M4)

General characteristics

* Crew: One
* Length: 7.55 m (24 ft 9¼ in)
* Wingspan: 11.0 m (36 ft 1 in)
* Height: 3.20 m (10 ft 6 in)
* Wing area: 17.8 m² (191.6 ft²)
* Empty weight: 1,216 kg (2,681 lb)
* Loaded weight: 1,705 kg (3,759 lb)
* Max takeoff weight: 1,822 kg (4,017 lb)
* Powerplant: 1× Nakajima Kotobuki 41 9-cylinder radial engine, 585 kW (785 hp) at 3,000 m (9,840 ft)

Performance

* Maximum speed: 440 km/h (237 knots, 273 mph) at 3,000 m (9,840 ft)
* Range: 1,200 km (649 NM, 746 mi)
* Service ceiling: 9,800 m (32,150 ft)
* Rate of climb: m/s (ft/min)
* Wing loading: 95.8.7 kg/m² (19.6 lb/ft²)
* Power/mass: 0.34 kW/kg (0.21 hp/lb)

Armament

* Guns: 2 × 7.7 mm Type 97 machine guns(0.303 in) fuselage-mounted machine guns


http://www.combinedfleet.com/ijna/a5m.htm
NEC JACTANTIA NEC METU ("zonder woorden, zonder vrees")

Avatar:De Siciliaanse vlag,oorspronkelijk uit 1282,de triskelion (trinacria) in het midden,is van oorsprong een oud Keltisch zonnesymbool.


Avatar gebruiker
Tandorini
Generaal
Generaal
 
Berichten: 2759
Geregistreerd: 30 mei 2008, 23:18

Keer terug naar Carrier vliegtuigen.

Wie is er online

Gebruikers op dit forum: Geen geregistreerde gebruikers. en 1 gast