Nakajima PA / Ki-11 / PE / Ki-27 / Type 97

Nakajima’s chief designer Yasumi Koyama had evolved an advanced single seat fighter from the company’s unsuccessful PA or Ki-11 low-wing monoplane prototype during 1934. While this private -venture low wing cantilever monoplane was still under development, Japanese army air headquarters issued a requirement to three major aircraft manufacturers, including Nakajima, for a similar aircraft in mid-1935. Nakajima responded with a single-seat monoplane fighter derived from the company’s Type P.E., which it had started to develop as a private venture.

The Ki 11 first flew in July 1936; the first prototype Ki 27, built to the official requirement, flew three months later. They differed only in detail, both being powered by a 650hp Nakajima Ha la radial engine and having a fixed, spatted cantilever single strut undercarriage. The Ki 27 had a redesigned and fully enclosed pilot’s cockpit canopy, and there were changes in the engine cowling, wheel spats and fin and rudder. A second Ki 27 prototype flew in December 1936, followed by ten pre-production aircraft. Different wing forms were tested and the Ki 27s were flown against rival prototypes Kawasaki’s Ki 28 and Mitsubishi’s Ki 33 developed from the navy A5M carrier fighter. Although achieving a maximum speed of’467 km/h (290 mph) at 4000 m (13 120 ft), it was still 15 km/h (10 mph) slower than the Ki 28 and took 28 seconds longer than its rival to reach 5000 m (16400 ft). The Ki 27 was nevertheless preferred to the Kawasaki fighter because of its outstanding manoeuvrability, due in part to the remarkable lightness of the structure and to the special aerofoil section developed by Koyama’s team.

Pre-production Ki 27s had a wing with span increased to 11.31 m (37 ft 1 in) which became standard on Ki 27a production aircraft. These appeared from December 1937 onwards, designated as the Army Type 97 Fighter. The standard engine was the Ha 1b developing 780 hp at 2900 m (9510 ft).

Nakajima Ki-27 Article

The original allied name assigned to the Ki.27 met in China by the CBI, “Abdul” was also called “Nate” by Col. MacCoy. The name Abdul was still caried in Naval recognition manual as late as February 1943. It was finally dropped in favour of the officially adopted “Nate”.

From spring 1938 Ki 27a fighters flew in northern China, and before the end of 1938 six Sentais (groups) newly established by the army were fully equipped with the Ki 27a. The Ki 27a model was, however, soon phased out of production in favour of Ki 27b, which had a wholly glazed pilot’s canopy and provision for two 130 litre (29 Imp gal) slipper type underwing drop tanks or four 25 kg (55 1b) bombs.

Ki.27a

Ki 27s were again in action in May 1939 when fighting broke out between Japanese and Soviet troops at Nomonhan along the border with Outer Mongolia. About 200 were ultimately engaged in full scale air battles with Soviet Polikarpov I 15bis biplanes and I 16 monoplanes. The Japanese acquitted themselves well in a most bloody conflict, and claimed many victories. The highest score of 58 enemy aircraft destroyed was claimed by Sergeant Shinobara of the 11th Sentai.

The poor state of the Allied air forces in the Far East in 1941 42 allowed Nakajima’s nimble fighter, despite its poor armament of twin synchronized 7.7 mm (0.303 in) Type 89 machine guns, to control the air over Burma, the Philippines and the Dutch East Indies. British, American, Australian and Dutch pilots all acquired a healthy respect for ‘Nate’, as the type was codenamed by the Allies, and they were careful to avoid getting entangled with it in an old style close dogfight. The Ki 27 achieved the distinction of shooting down the first Allied aircraft of the Pacific war, when an aircraft of the 1st Sentai destroyed a Consolidated Catalina flying boat of No 205 Squadron RAF while covering Japanese landings on the Malayan coast.

With the advent of newer types, Ki 27s were relegated to advanced training or home defence. In the latter role they were at a stroke rendered impotent when the Boeing B 29 Superfortress came on the scene, and as the war drew to a close, Ki 27s were adapted as suicide attackers, a number of their pilots sacrificing themselves while endeavouring to crash into enemy ships or land positions carrying a 500 kg (1100 lb) bombload.

Mansyu Kikoki Seizo K K (Manchurian Aeroplane Manufacturing Company), based in the Japanese puppet state, built 1379 Ki-27s at its Harbin factory as against 2020 built by Nakajima up to December 1942, when all production by the parent firm ceased. Production included two Ki 27 Kai prototypes, even lighter than the standard machine, which reached a maximum of 475 km/h (295 mph) during tests in summer 1940.

In 1942 Mansyu redesigned the Ki 27 as an advanced trainer which went into production the same year as the Army Type 2 Advanced trainer.

Ki-27a
Engine: 1 x Nakajima Ha-1b, 529kW
Max take-off weight: 1790 kg / 3946 lb
Empty weight: 1110 kg / 2447 lb
Wingspan: 11.31 m / 37 ft 1 in
Length: 7.53 m / 24 ft 8 in
Height: 3.25 m / 10 ft 8 in
Wing area: 18.55 sq.m / 199.67 sq ft
Max. speed: 470 km/h / 292 mph
Ceiling: 12250 m / 40200 ft
Range w/max.fuel: 625 km / 388 miles
Armament: 2 x 7.7mm machine-guns
Crew: 1

Ki-27b
Engine: Hitachi Ha-1b, 750 hp
Wing span: 11.31 m / 37 ft 1 in
Wing area: 18.56 m2
Length: 7.53 m / 24 ft 8 in
Height: 3.28 m / 9 ft 2 in
Empty weight: 1110 kg / 2447 lb
Loaded weight: 1547 kg / 3946 lb
Max speed: 470 km/h at 3500 m
Max speed: 286 mph at 16,400 ft
Time to 5000m: 5m 22s
Service ceiling: 12,250 m
Service Range: 627 km
Max range: 1100 km
Armament: 2 x 7,7-mm Type 89 machine guns
Crew: 1
Bombload: 220 lb

Nakajima Ki-27 NATE

Nakajima J5N Tenrai

Designed by Katsuji Nakamura and Kazuo Ohno and built to an 18-Shi specification for a high-speed single-seat interceptor fighter, the Nakajima J5N1 Tenrai (Heavenly Thunder) began flight tests in July 1944.

A mid-wing monoplane with a raised canopy over the pilot’s cockpit, it was powered by two 1484kW Nakajima NK9H Homare 21 radials and had a maximum speed of 597km/h. Armament comprised two 30mm and two 20mm cannon.

Six aircraft were built, four were lost in crashes or on the ground and none were used operationally. As performance was disappointingly below specification no production resulted.

Nakajima J5N “Tenrai”
Engines: 2 x Nakajima NK9H “Homare-21”, 1484kW
Max. speed: 597 km/h / 371 mph
Armament: 2 x 30mm cannons, 2 x 20mm cannons
Crew: 1

Nakajima J5N Tenrai

Nakajima 18-Shi / G8N Renzan

Developed as the Experimental 18-Shi Heavy Bomber Renzan (Nakajima G8N1), this was a very advanced long-range bomber powered by four 1491kW Nakajima Homare 24 radials which gave it a maximum speed of 592km/h at 8000m. Maximum range was 7465km. Armament consisted of six 20mm cannon in twin power-operated dorsal, ventral and tail turrets, two 13mm machine-guns in a power-operated nose turret, and single machine-guns of similar calibre in port and starboard beam positions. A maximum bombload of 4000kg could be carried over short ranges.

Four prototypes were built up to June 1945, but the proposed production programme was disrupted by Allied bombing and was abandoned when the navy’s role became defensive rather than offensive. These prototypes were allocated the Allied codename ‘Rita’.

G8N1
Engine: 4 x Nakajima NK9K-L “Homare-24”, 1500kW
Wingspan: 32.54 m / 106 ft 9 in
Length: 22.94 m / 75 ft 3 in
Height: 7.2 m / 23 ft 7 in
Wing area: 112 sq.m / 1205.56 sq ft
Max take-off weight: 26800-32150 kg / 59084 – 70879 lb
Empty weight: 17400 kg / 38361 lb
Max. speed: 590 km/h / 367 mph
Cruise speed: 390 km/h / 242 mph
Ceiling: 10200 m / 33450 ft
Range: 4000 km / 2486 miles
Range w/max.fuel: 7500 km / 4660 miles
Armament: 6 x 20mm cannons, 4 x 12.7mm machine-guns, 1000-4000kg of bombs

Nakajima G8N Renzan / RITA

Nakajima G5N Shinzan

The first application of the Nakajima Mamoru engines was on the first prototype of the G5N1 Genzan, first flying on April 10, 1941. The G5N1 had been designed on the basis of the Douglas DC-4E as Japan’s first four-engine bomber, and proved to be a disappointment. These problems were compounded by the unreliability of the early Mamoru engines, which had to be de-tuned and left the G5N1 underpowered. The G5N1’s maiden flight was on 10 April 1941, and a further four prototypes were built with the Mamoru. In an attempt to salvage the project, two additional airframes were fitted with 1,530 hp Mitsubishi MK4B 12 “Kasei” engines and redesignated G5N2s. Although the Mitsubishi engines were more reliable than the original Mamoru 11s, further development was halted. Of the six completed Shinzans, four of them (two G5N2s and two G5N1s re-engined with the Kasei 12) were relegated for use as long-range Navy transports under the designation Shinzan-Kai Model 12 Transport G5N2-L.

First spotted by an Intelligence Officer from AAF Headquarters in Washington, the bomber was coded ‘Liz’ after his daughter.

G5N1
Engine: 4 x Nakajima NK7A Mamoru-11, 1400kW
Max take-off weight: 28150-32000 kg / 62060 – 70548 lb
Empty weight: 20100 kg / 44313 lb
Wingspan: 42.12 m / 138 ft 2 in
Length: 31.02 m / 101 ft 9 in
Wing area: 201.8 sq.m / 2172.16 sq ft
Max. speed: 420 km/h / 261 mph
Cruise speed: 370 km/h / 230 mph
Ceiling: 7450 m / 24450 ft
Range: 4260 km / 2647 miles
Crew: 7
Armament: 2 x 20mm cannons, 4 x 7.7mm machine-guns
Bombload: 2000-4000kg

G5N2
Engines: 4 x 1,530 hp Mitsubishi MK4B 12 Kasei
Wingspan: 42.12 m / 138 ft 2 in
Length: 31.02 m / 101 ft 9 in
Wing area: 201.8 sq.m / 2172.16 sq ft

G5N2-L Shinzan-Kai Model 12
Engines: 4 x 1,530 hp Mitsubishi MK4B 12 Kasei
Wingspan: 42.12 m / 138 ft 2 in
Length: 31.02 m / 101 ft 9 in
Wing area: 201.8 sq.m / 2172.16 sq ft

Nakajima G5N Shinzan / LIZ

Nakajima Ki-8

Although the Imperial Navy had discarded the two-seat fighter requirement that had resulted in the NAF-1 and -2, western developments in this category of aircraft stimulated some interest on the part of the Army to which, in 1933, Nakajima offered an advanced company-funded two-seat fighter project. Designed by Shigejiro Owada and Toshio Matsuda, and assigned the designation Ki-8 by the Army, the aircraft was an all-metal low-wing cantilever monoplane with a monocoque fuselage and spatted cantilever fixed under-carriage. Powered by a Nakajima Kotobuki 3 engine rated at 710 hp for take-off and carrying an armament of two fixed forward-firing 7,7-mm guns and one 7,7-mm gun on a flexible mount, the Ki-8 was conceptually advanced and five proto¬types were built between March 1934 and May 1935. Army evaluation revealed stability and other problems, and al¬though these were subsequently rectified, doubts concerning the practicability of the two-seat fighter concept led to the discontinuation of further development.

Nakajima J1N Gekko

Work on the Nakajima J1N Gekko (Moonlight) design began in 1938 to a Navy specification for a long range escort fighter, and the prototype J1N1 made its maiden flight in May 1941. Flight test revealed several factors against its suitability as a fighting aircraft but in July 1942 it was ordered into production for the reconnaissance role as the J1N1-C.

When first encountered in action during the Solomons campaign the aircraft was mistakenly thought to be a Naval ‘Nick’. Codenamed ‘Irving’ by the Allies covering many different model, it soon narrowed down to the reccon and night fighter versions, J1NC-1 Type 2 and J1N1-S Gekko respectively.

As night air attacks were stepped up by the Americans it was the commanding officer of the 251st Kokutai, Commander Yasuna Kozono, then based at Rabaul, New Guinea, who first suggested adaptation of the J1N as a night-fighter by installing two 20mm cannon in the observer’s cockpit, fixed to fire obliquely forward and upward at an angle of 30 degrees, and another pair firing forward and downward. When two Consolidated B-24s were quickly destroyed, the modifications came to the attention of the Japanese naval staff and an order was placed with Nakajima to go ahead with a dedicated night-fighter version, designed and built as such from scratch.

These were followed by a few turret-mounting J1N1-F and later by the J1N1-S Gekko, built from the onset for night-fighting, some later bearing primitive centimetric AI radar in the closing stages of the war, and some aircraft also carried a small nose searchlight.

This version, the J1N1-S, entered production in August 1943 and continued until December 1944, during which period a total of 420 J1Ns were produced, the great majority of them J1N1-S night-fighters. These differed from the earlier reconnaissance version in having the crew reduced from three to two, the observer’s cockpit being eliminated and faired over. All aircraft retained the upward-firing cannon, but the downward firing guns (found difficult to aim and seldom used) were omitted from later aircraft, while a third upper gun and a forward-firing 20mm cannon was fitted in the J1N1-Sa.

Total production of the J1N, including prototypes, amounted to 479. Some of these were employed on bombing duties with an offensive load of up to 2432 lb.

In service with the 251st, 302nd and 322nd Kokutais, the J1N1-S night-fighters proved fairly effective against the B-24, which was not in any case well-suited to night operations, but with the appearance of the Boeing B-29 the Japanese night-fighters proved too slow and were seldom able to make more than a single firing attack. Most of them were expended during the final months of the war when, equipped to carry two 250kg bombs, they were employed in kamikaze attacks against ground targets.

J1N1-S
Engines: 2 x Nakajima “Sakae-21”, 843kW / 1130 hp
Wingspan: 16.98 m / 55 ft 9 in
Length: 12.77 m / 41 ft 11 in
Height: 3.99 m / 13 ft 1 in
Wing area: 40 sq.m / 430.56 sq ft
Max take-off weight: 8185 kg / 18045 lb
Empty weight: 4850 kg / 10692 lb
Max. speed: 507 km/h / 315 mph at 19,030 ft
Service ceiling: 9320 m / 30600 ft
Normal range: 1584 mi
Range w/max.fuel: 3780 km / 2349 miles
Armament: 4 x Type 99 20mm cannons
Crew: 2

Nakajima J1N Gekko / IRVING

Nakajima B6N Tenzan

At a time when the triumphs of the B5N were still almost three years in the future, the Japanese navy issued a specification for a replacement, recognizing that only limited overall design improvement of the B5N could be achieved in the B5N2. Accordingly design went ahead in 1939 of the Nakajima B6N and, despite the Navy’s preference for the Mitsubishsi Kasei radial, a Nakajima Mamoru was selected for the prototype which flew on 14 March 1941, demonstrating several problems, notably the poor engine reliability. With the delay of 2 years, by 1943 the engine had improved to the point where serial production was allowed to start, but after only 133 B6N1s had been delivered the Navy ordered the switch to the 1,850 hp (1380 kW) Mitsubishi MK4T Kasei 25. The rest of the 1,268 B6N2s were Kasei powered.

B6N2

Superficially the B6N Tenzan (Heavenly Mountain) resembled the earlier aircraft, but the much increased power and torque of the big engine and four-blade propeller was found to impose considerable directional stability problems, demanding that the vertical tail surfaces be offset to one side. Flight trials dragged on, and were further delayed by troubles during carrier acceptance tests. Then Nakajima was ordered to stop production of the Mamoru engine, so modifications had to be introduced to suit installation of the Kasei.

In due course B6N1 aircraft (of which only 133 were built) were embarked in the carriers Shokaku, Taiho, Hiyo, Junyo and Zuikaku, and took part in the Battle of the Philippine Sea of June 1943, many being lost when the three Shokaku, Taiho, and Hiyo were sunk.

In that month production started of the slightly improved B6N2 (of which 1,133 were produced before the end of the war), but the heavy losses among Japanese carriers resulted in the ‘Jill’ being largely deployed ashore, particularly after the Battle of Leyte Gulf. Thereafter many BsNs were consigned to the kamikaze role.

B6N2

B6N2
Engine: 1 x Mitsubishi MK4T “Kasei-25”, 1850 hp
Wingspan: 14.9 m / 48 ft 11 in
Wing area: 37.2 sq.m / 400.42 sq ft
Length: 10.87 m / 35 ft 8 in
Height: 3.8 m / 12 ft 6 in
Empty weight: 3010 kg / 6636 lb
Max take-off weight: 5650 kg / 12456 lb
Max. speed: 480 km/h / 298 mph at 16,076 ft
Ceiling: 9040 m / 29650 ft
Service ceiling: 26,660 ft
Range w/max.fuel: 3045 km / 1892 miles
Armament: 1 x 13 mm, 2 x 7.9mm machine-guns
Bomb load: 1 x 1764 lb torpedo or 6 x 220 lb bombs
Crew: 3

Nakajima B6N Tenzan / JILL

Nakajima B5N

Designed to a 1935 requirement, and already in service for four years when Japan entered the war, the prototype B5N first flew in January 1937. A low-wing three-crew monoplane with inwards-retracting wide-track landing gear, powered by a 770 hp Hikari engine, and entered production as a 1000 hp Nakajima Sakae 11-powered light or torpedo-bomber. The following year production B5N1 aircraft were embarking in Japan’s carriers and shore-based units were deployed in China.

Nakajima B5N Article

In 1939 the improved B5N2 appeared with a more powerful Sakae 11 engine in a smaller cowling, although armament and bombload were unchanged, and this version remained in production until 1943.

Many were converted to B5N1-K trainers when production switched to B5N2.

When Japan attacked the USA the B5N2 had wholly replaced the B5N1 with operational units, and 144 B5N2s were involved in the attack on Pearl Harbour, and within the next 12 months aircraft of this type sank the American carriers USS Hornet, Lexington and Yorktown.

B5N2

Given the reporting name ‘Kate’ by the Allies, with its defensive armament of a single machine-gun and laden with a large bomb or torpedo, the B5N began to suffer very heavily, and although the type was fully committed during the Solomons campaign the survivors were withdrawn from combat after the Philippine battles of 1944.

Thereafter, on account of their excellent range, they were assigned to antisubmarine and maritime reconnaissance duties in areas beyond the range of Allied fighters. Production of all B5Ns reached 1,149.

B5N2

Gallery

Nakajima B5N1
Engine: 1 x 840 hp Nakajima Hikari 3
Prop: 3 blade Constant speed
Wingspan: 50 ft 11 in
Length: 33 ft 9.5 in
Height: 12 ft 1.5 in
Wing area: 405.8 sq.ft
Wing loading: 20.1 lb/sq.ft
Loaded weight: 4640 lb
Max weight: 8150 lb
Max speed: 229 mph at 6,500 ft
Cruise speed: 159 mph at 6500 ft
Climb to 10,000 ft: 8 min
Service ceiling; 24,280 ft
Normal range: 590 nm
Max range: 1220 nm

Nakajima B5N2
Engine: 1 x Nakajima NK1B “Sakae”, 746kW
Wingspan: 15.52 m / 50 ft 11 in
Length: 10.3 m / 33 ft 10 in
Height: 3.7 m / 12 ft 2 in
Wing area: 37.7 sq.m / 405.80 sq ft
Max take-off weight: 4100 kg / 9039 lb
Empty weight: 2279 kg / 5024 lb
Max. speed: 378 km/h / 235 mph
Ceiling: 8260 m / 27100 ft
Range w/max.fuel: 1990 km / 1237 miles
Armament: 1 x 7.7mm machine-guns, 800kg of bombs
Crew: 3

Nakajima B5N KATE

Nakajima NC / Type 91

A Japanese army requirement of March 1927 for a new single-seat fighter successor for the Ko-4 (Nieuport-Delage NiD 29) was contested by Nakajima, Kawasaki and Mitsubishi. All the designs were parasol-wing monoplanes developed in Japan by teams wholly or partly led by Europeans, in the case of Nakajima the French engineers Mary and Robin from Dewoitine leading designers Shigejiro Owada and Tei Koyama. Structural failure of the Mitsubishi prototype led to severe testing of the survivors, which were then also eliminated.

The Nakajima: prototype, company designation NC, had a slim tapering monocoque fuselage, an uncowled Jupiter VI nine-cylinder radial engine, and elaborate strut bracing connecting wings, fuselage and the wide-track landing gear. Two prototypes were completed in May and June 1928 respectively, but structural testing led to rejection by the Army. The contest was, in the event, cancelled but Nakajima persevered with the design as a company-funded venture and built six more prototypes armed with two 7,7-mm machine guns be¬tween 1929 and 1931.

The final two of these prototypes were, in fact, of an essentially new design, retaining no more than the rear fuselage of the preceding prototypes. These were to serve as a basis for the series Type 91 fighter. The last of the series being tested extensively by the Japanese army and accepted for production as the Army Type 91 Fighter Model 1.

Type NC No.7

Retaining the company appellation NC, the sixth prototype so designated was of fundamentally different design and powered by a supercharged 520 hp Bristol Jupiter VII radial. New wings of smaller area incorporated an internal (jettisonable) fuel tank to port replacing the podded tank of preceding prototypes. The engine was enclosed by a Townend ring, the diameter of the forward fuselage was increased, both fore and aft main bracing struts were attached to the fuselage, the tail surfaces were redesigned, the cross-axle gave place to one of split type and the guns were repositioned.

This was ordered into production by the Army as the Type 91, deliveries commencing late 1931, but service introduction being delayed by C of G and directional stability problems. A total of 320 fighters of this type was built by the parent company (and approximately 100 more by Tachikawa), the initial version subsequently becoming the Type 91-1 with the appearance of a version powered by a Jupiter derivative, the Nakajima Kotobuki 2 of 580 hp. A prototype of this variant, the Type 91-2, was completed in July 1934, this being followed by 22 series aircraft, production terminating in September 1934 with the 450th aircraft.

Introduced from 1932 onwards, the Type 91s were deployed in action with the four squadrons of the 11th Air Battalion operating with the army Kanto Command in Manchuria against the Chinese. In. 1933 the Type 91 was the principal army fighter and constituted the standard equipment for the newly formed air wings (or Hiko Rentai). The Type 91 remained in service until succeeded by the Kawasaki Type 95 in 1936-37.

A Type 91 was converted for carrier operations and with spatted wheel fairings was submitted for the navy 7-Shi experimental fighter competition, but was rejected. The only other modification from standard army configuration was the use of a three-bladed propeller.

One experimental example was fitted with a Kotobuki 5 engine.

Type 91-1
Engine: Bristol Jupiter VII, 520 hp.
Max speed: 186 mph (300 km/h).
Endurance: 2 hrs.
Time to 9,845ft (3000m): 40 min.
Empty weight: 2,370 lb (1 075 kg).
Loaded weight: 3,373 lb (1 530 kg).
Span: 36 ft 1 in (11.00 m).
Length: 23 ft 9.75 in (7.26 m).
Height: 9 ft 1.8 in (2,79 m).
Wing area: 215.28 sq ft (20,00 sq.m).

Type 91-2
Engine: Nakajima Kotobuki 2, 580 hp / 433kW
Wingspan: 11 m / 36 ft 1 in
Length: 7.3 m / 23 ft 11 in
Height: 3 m / 9 ft 10 in
Wing area: 20 sq.m / 215.28 sq ft
Max take-off weight: 1500 kg / 3307 lb
Empty weight: 1075 kg / 2370 lb
Max. speed: 300 km/h / 186 mph
Ceiling: 9000 m / 29550 ft
Range: 500 km / 311 miles
Armament: 2 x 7.7mm machine-guns
Crew: 1