Sunday, 5 October 2025

Kawasaki Ki-48 "Lily" and "Ne0"

The sole prototype Kawasaki Ki-48-II "Lily" with the Ne0 ramjet engine hanging under its fuselage. The pod beneath the fuselage was hollow, with the fuel and nozzle housed within the bomb bay.

As the Second World War intensified, the front lines demanded higher-performance propeller aircraft, leading to increased interest in jet engines. Almost simultaneously with the Navy commencing development of its turbojet engine, designated ‘TR’, the Army and the University of Tokyo Aeronautical Research Institute also established specialised departments and began research.
Engineer Hayashi Teisuke was appointed from the Army's Second Aeronautical Research Institute to lead the jet engine development effort on a one-year contract basis. In mid-November 1942, a team led by Hayashi, comprising nine subordinates from Kawasaki, commenced development. Alongside the main engine concepts proposed by the Tokyo Aviation Research Institute – the Ne* 101 motorjet and the Ne 201 turboprop – it was decided to develop motorjets and turbojets for auxiliary engines. As the characteristics of the engine types were unknown, it was decided to produce both compressor types: axial-flow and centrifugal:
1. ‘Ne1’ two-stage axial-flow motor jet
2. ‘Ne2’ single-stage centrifugal motor jet
3. ‘Ne3’ three-stage axial-flow turbojet
4.  ‘Ne4’ single-stage centrifugal turbojet, and
5.  ‘Ne0’ ramjet for fundamental research.
The Ne1 and Ne2 were auxiliary engine variants of the Caproni Campini-type engine-jet. They were intended for installation either aft of the fuselage in single-engine propeller fighters or behind the engine nacelle in twin-engine propeller aircraft.
The Ne3 and Ne4 were both primarily targeted for installation in single-engine or twin-engine propeller-driven fighters.
Work proceeded at considerable speed, with drawings largely completed within approximately six months. 

The Kawasaki Ne0 ramjet engine.

The Ki-61 "Hien" was proposed as the primary candidate for a test aircraft**, with the Ki-45 Kai "Toryu" twin-engine fighter as the second choice. However, at a time when even a single front-line aircraft was desperately needed, neither could be obtained. Consequently, the slow-speed Ki-48 Type II twin-engine bomber "Lily" had to be used.
To minimise airframe modifications, a design utilising bomb racks to suspend the engine beneath the fuselage was developed with the cooperation of aircraft designers Imachi Isamu and Kitano Jun.

Illustration from Encyclopedia Vol. #IV

Ne0 was finished in November 1943, and on the morning of 23 December 1943, test pilot Kataoka Saizaburo*** took off from Kawasaki with engineers Hayashi and Nozu aboard. However, ignition of the combustor failed, necessitating a landing. After servicing the ignition plug, they took off again in the afternoon.
This time, the combustor ignited easily. The aircraft accelerated, delivering considerable shock to the passenger seats and momentarily causing the nose to pitch up. It then maintained high-speed cruise at an altitude of 800 to 1000 metres for approximately ten minutes before landing.
Subsequent multiple flights reportedly yielded preliminary results. Though abandoned after flight testing concluded, the entire airframe was transferred to the Army's Second Aeronautical Research Institute in July 1944. 
Following Ne0 testing, research focus shifted to two of the four Ne1 to Ne4 variants—Ne3 and Ne4—with ground-running tests conducted on prototypes. However, due to the worsening war situation and the acquisition of engine data from Germany, all development of these Kawasaki jet engines was suspended during the prototype consolidation in July 1944. Consequently, no aerial tests were conducted before the war's end.

Specifications

Ne0
• Type: Ramjet
• Overall length: 2,100mm
• Maximum cross-sectional diameter: 600mm
• Thrust: 60kg (altitude 2,800m)
• Air flow rate: 8.1kg/s (altitude 2,800m)
• Compression ratio: 1.12 (altitude 5,800m, 550km/h)

Ne1
• Type: Motorjet
• Compressor: Two-stage axial flow, contra-flow type
• Length from rear edge of impeller to jet nozzle: 1,050mm
• Outer casing diameter: 600mm
• Thrust: 185.5kg × 2 (altitude 2,800m)
• Airflow: 10.4kg/s (altitude 2,800m)

Ne2
• Type: Motorjet
• Compressor: Single-stage centrifugal
• Thrust: 150kg (planned)

Ne3
• Type: Turbojet
• Overall length: 2,321mm
• Casing outer diameter: 760mm
• Total weight: 309 kg + (casing weight)
• Compressor: 3-stage axial-flow
• Turbine: 1-stage axial-flow
• Thrust: 348 kg (altitude 2,800 m)
• Air flow rate: 14.9 kg/s (altitude 2,800 m)
• Compression ratio: 1.71 (5,800 m, 550 km/h)
• Rotational speed: 8,300 rpm (altitude 2,800 m)

Ne4
• Type: Turbojet
• Overall length: 1,700 mm
• Casing outer diameter: 750 mm
• Total weight: 270 kg + (casing weight)
• Compressor: Single-stage centrifugal
• Turbine: Single-stage axial
• Thrust: 276 kg (altitude 2,800 m)
• Airflow: 10.35 kg/s (altitude 2,800 m)
• Compression Ratio: 1.98 (5,800 m, 550 km/h)
• Rotational Speed: 1,100 rpm (altitude 2,800 m)

*"ネ" (NE) was a common designation used by both the IJAAF and the IJNAF. At the time, both jet and rocket engines were collectively referred to as "燃焼ロケット" ("NEnsho roketo" combustion rockets).

**One can only imagine what a "Hien" would look like with a jet engine on its tail.

***A test pilot for the Imperial Japanese Army Air Force, he was responsible for the maiden flights of prototypes such as the Ki-61-II "Hien" and the Ki-78, manufactured by Kawasaki Aircraft. During the Ki-78 (Ken-3) test flight in January 1944, he recorded a top speed of 699.9 km/h, which remained Japan's speed record until the end of the war.

Tuesday, 30 September 2025

Kobeseiko "Te-Go" Experimental Observation Aircraft


Designed by Professor Miki Tetsuo of the Department of Aeronautics, Faculty of Engineering, Osaka Imperial University, at the request of the Army, as a short take-off and landing aircraft for artillery spotting by the Army Artillery Corps. As it was outside the jurisdiction of the IJAAF, it was not assigned a Ki number. It featured a distinctive high-wing monoplane configuration, equipped with automatic leading-edge slats spanning the entire main wing, trailing-edge Fowler flaps, and ailerons doubling as flaps. To achieve a large wing angle of attack during take-off and landing runs, the main landing gear was raised high. Large windows were fitted to the fuselage to provide a wide field of view. 
The wings were wooden with fabric covering and could be folded rearward. The fuselage featured a mixed wooden and metal frame covered in fabric, with only the nose section clad in light metal. Priority was given to short take-off and landing performance for use from hastily constructed frontline airfields, riverbanks, open spaces, and roads. Seating was arranged in a single file.
The engine was the same type as that fitted to the Kayaba "Ka-go" Type 1 observation autogyro, the Kobe Steel Argus As-10 24OH. For the "Te-go" observation aircraft, Kobe Steel also manufactured the airframe, with the prototype completed in 1942. However, it had a landing gear failure during test flights. Consequently, the Army adopted the "Ka-go" observation autogyro for this role, and development of the "Te-go" was cancelled.
Plans also existed for a three-seat Army artillery observation aircraft (abbreviated RGK), but only the design was completed and no actual aircraft were built. It would be a large observation aircraft equipped with the Nakajima ‘Kotobuki’ Type 3 5501P engine, with a wingspan of 21.00m, length 12.80m, and height 2.70m.

General characteristics
Single-engine, high-wing monoplane, land-based aircraft
Crew: 2
Length: 9.50m
Height: 3.00m
Wingspan: 13.00m
Wing area: 20sq m
Maximum take-off weight: 1,130 kg
Wing loading: 56kg/sq m
Power loading: 4.52kg/hp
Powerplant: 1 X Kobe Steel Argus As-10 air-cooled inverted V-8, nominal output 240 hp, take-off output 250 hp.
Propeller: Wooden fixed-pitch, 2-bladed, diameter 2.75 m

Performance
Maximum speed: 180 km/h
Endurance: 6 hours
Service ceiling: 8,2 80m (27,165 ft)
Armament: One 7.7 mm flexible machine gun (mounted above rear seat, retractable, with two spare magazines)

Illustration from "Nihon Rikugun Shisakuki Taikan" (All the Experimental Aircraft in Japanese Army), by Akimoto Minoru, Kantosha 2008

Monday, 29 September 2025

Mitsubishi Army Experimental "Tobi" Reconnaissance Aircraft (Company designation 2MR1)


In 1926, the IJAAF sought competitive proposals from Nakajima, Kawasaki, Ishikawajima, and Mitsubishi to replace the Type Otsu 1 Reconnaissance Aircraft (Salmson 2-A.2s). Mitsubishi, with the assistance of Dr Alexander Baumann, a professor at Stuttgart University, and former designer of Riesenflugzeug for Zeppelin-Staaken, assigned Nobushiro Nakata as chief designer and Satsuo Tokunaga as his assistant. The result was a radical design for a sesquiplane, having the upper wing set unusually high above the slender fuselage, connected with a unique type of center-section and interplane struts. As one of the Mitsubishi bird series projects in 1925-27, this aircraft was given the name “Tobi” (black kite ).
The first prototype was completed in July 1927. In the hands of test pilot Jiro Itoh the aircraft achieved speed of 227km/h (123kt) faster than the Army's specified 200km/h (108kt). Mitsubishi had high expectations for the new aircraft, but during an official qualifying test flight by the Army at Tokorozawa, an undercarriage shock strut failed and during the landing the aircraft was badly damaged and eliminated from the competition. The Nakajima and Ishikawajima entries also failed, but the Kawasaki aircraft met the requirements and was accepted as the Type 88 Reconnaissance Aircraft (KDA-2). 

General characteristics
Single-engine sesquiplane with large gap. Metal fuselage structure with wood and metal wings, fabric covered with some plywood and thin metal on the forward fuselage.
Crew: 2 in open cockpits
Length: 9.55m (31ft 4in)
Height: 4.35m (14ft 31/2in)
Wingspan: 17.40m (57ft)
Wing area: 50sq m (538.213sq ft), upper 34.50sq m (371.367sq ft), lower 15.50sq m (166.846sq ft)
Empty weight: 1,350kg (2,9761b)
Gross weight: 2,500kg (5,5111b)
Wing loading: 50kg/sq m (10.2411b/sq ft)
Power loading: 3.5kg/hp (7.71b/hp)
Powerplant: 1 X 450-600hp Mitsubishi-Hispano-Suiza twelve-cylinder vee water-cooled engine, driving a Mitsubishi-Reed fixed-pitch two-bladed metal propeller

Performance
Maximum speed: 123kt (142mph) at 5,000m (16,404ft)
Endurance: 6 hours
Service ceiling: 8,2 80m (27,165 ft)

Armament
Guns: Two forward-firing fixed 7.7mm machine-guns and twin dorsal flexible 7.7mm machine-guns

*Note that the Wiki entry for the "Mitsubishi Experimental Tobi-type Reconnaissance Aircraft" links to the IJNAF Mitsubishi 2MR Carrier-based Reconnaissance Aircraft, a completely unrelated aircraft type which first flew in 1922.

Sunday, 28 September 2025

Experimental 7-Shi Carrier Attack Aircraft (Nakajima B4N1, Y3B)


In April 1932, the Navy issued instructions to Mitsubishi and Nakajima to prototype a new carrier-based attack aircraft to replace the unpopular Type 89 Carrier Attacker. Nakajima, with Engineer Yoshida Takao as chief designer, developed the distinctive biplane Y3B equipped with the newly designed “Hikari” 73O engine. Two prototypes were built in 1933 and submitted for Navy evaluation. This aircraft featured a Gal-type upper wing and an inverted Gal-type lower wing, with the central section crossing in an X-shape relative to the slender fuselage. Furthermore, the landing gear struts were cantilevered from the lower wing's bend, representing an extremely bold structural design. The fuel tanks were exposed and removable, mounted on both sides of the fuselage, similar to those on the Nakajima E4N2 Reconnaissance Seaplane and the Nakajima A2N Carrier Fighter Model 2. At the time, the development of tri-seat carrier-based attack aircraft was a major challenge not only for Mitsubishi and Nakajima but also for Aichi and the Naval Technical Arsenal. Particularly, the selection of a reliable, high-horsepower engine proved difficult, preventing the establishment of a definitive design. Two prototypes were built in 1933 with the short designation B4N1*, and delivered to the Navy for evaluation but they failed to win Navy approval. Mitsubishi submitted its 7-Shi Carrier Attack Aircraft but it crashed on takeoff due to engine failure. Because of these failings, the Navy began with a new design competition for a 9- Shi Carrier Attack Aircraft.

Check this amazing scratch-built model here.

General characteristics
Crew: 3 (pilot, navigator/bomb aimer and gunner)
Length: 10 m (32 ft 10 in)
Wingspan: 14 m (45 ft 11 in)
Height: 3.80 m (12 ft 6 in)
Wing area: 50.0 m2 (538 sq ft)
Empty weight: 2,000 kg (4,409 lb)
Gross weight: 3,800 kg (8,378 lb)
Powerplant: 1 × Nakajima Hikari 2 9-cylinder radial engine, 520 kW (700 hp)
Propellers: 3-bladed

Performance
Maximum speed: 220 km/h (140 mph, 120 kn)
Stall speed: 93 km/h (58 mph, 50 kn)
Endurance: 6 hr
Service ceiling: 5,500 m (18,000 ft)
Time to altitude: 12 minutes to 3,000 m (9,800 ft)

Armament
Guns: 1 × flexibly mounted 7.7 mm machine gun
Bombs: 1 × 800 kg (1,760 lb) torpedo, or 1 × 800 kg bomb, or 2 × 250 kg bombs

*Francillon, Model Art #327 and others mention that the designation was "B4N1", only Mikesh-Abe mention that it was "B3N1". Considering that the Mitsubishi entry in the 7-Shi competition was designated B4M1 agreed by everyone including Mikesh-Abe and that the officially adopted type was the B4Y1 (also agreed by everyone), it is safe to conclude that the "B3N1" designation mentioned in the Mikesh-Abe book was a missprint. The Wiki entry needs correcting...

Saturday, 27 September 2025

Nakajima Bulldog Fighter


Nakajima's design for a parasol-wing fighter, along with those of other companies competing for the Army's requirement for a new fighter, met with early uncertainties. Eventually, Nakajima's design was further developed and became the successful Army Type 91 Fighter, but in the interim, Nakajima, in 1930, bought the licence-manufacturing rights for the Bristol Bulldog. This aircraft was thought by Nakajima to be an ideal replacement for the ageing Type Ko 4 Fighters. Like the earlier N-35 Reconnaissance Aircraft, this project was supervised by the same French team headed by Andre Marie, assisted by Maxime Robin and others. Because this was a British-designed aircraft, Leslie G. Frise of the Bristol Aeroplane Co and his assistant H.W. Dunn were invited to Japan to assist. The first prototype was completed in June 1930, followed soon after by the second prototype. The design was based upon the Bristol Bulldog Mk. II, but differed by having each engine cylinder covered by separate fairings, the interplane struts were changed to the N type as used on the Bristol Bullpup, and struts were used to brace the tailplane. The Nakajima Jupiter engine was substituted for the Bristol-built Jupiter. After two prototypes were built, some of the parts were found to have insufficient strength for safe flight, therefore Nakajima Chikuhei grounded them. As a consequence, they were never submitted to the Army for evaluation; however, Nakajima's design for the parasol-wing Type 91 Fighter had by now achieved success. The two Bulldogs were eventually donated to the Navy, at the outbreak of the Shanghai Incident, for structural research purposes.

General characteristics
Single-engine single-seat fighter biplane. Metal structure with fabric covering.
Crew: Pilot in open cockpit.
Length: 7.54m (24ft 9in)
Span: 10.36m (34ft)
Height: 2.99m (9ft 91/2in)
Wing area: 28.5sq m (306.781sq ft)
Wing loading 56.1kg/sq m (11.51b/sq ft)
Power loading 3.55kg/hp (7.81b/hp)
Empty weight: 1,000kg (2,2041b)
Gross weight: 1,600kg (3,5271b)
Powerplant: 450-520hp Nakajima Jupiter VII nine-cylinder air-cooled radial engine, driving a two-bladed wooden propeller.

Performance
Maximum speed: 148kt (170.3mph) at 3,000m (9,843ft)
Climb to 5,000m (16,404ft) in 11 min
Service ceiling: 7,650m (25,098ft)

Saturday, 20 September 2025

Aichi B7A1 "Ryusei" (Grace) by Jan Voorbij


Aichi B7A1 "Ryusei" (Grace)
Dive bomber / Torpedobomber
Pre-production plane: 1 of 9 prototypes
Imperial Japanese Navy, Kougeki (attack) 5th Hikotai, 752nd Kokutai, April/May 1945 and later 1945 Katori Naval Air Base April 1945 till the end of May 1945, then moved to Kisarazu Naval Air base. Captured by US troops in August 1945.
Fujimi 7AF1, 1:72

- Jan Voorbij, Holand -

Thursday, 18 September 2025

Kawasaki Experimental Carrier Reconnaissance Aircraft


In March 1927, the Navy decided to manufacture an experimental aircraft funded by a program sponsored by the Kaibo Gikai (Maritime Defense Volunteer Association), and named the project: 'Research of Material for All-metal Aircraft'. Kawasaki was awarded the project by the Navy. It was to be a single-engine carrier reconnaissance aircraft having an all-metal structure with fabric covering. It had a fully cantilever parasol wing with marked sweepback, and large area slotted flaps, the first in Japan and probably the first in the world. At that time, no monoplane existed for carrier-based aircraft and there were certainly none with cantilever wings and slotted flaps. The fuselage was unusual being almost triangular in the cross section. The structure of the aircraft was heavily influenced by Dornier design practices. 
Design begun in March 1927 and completed in June 1928 under the leadership of Junichiro Nagahata and his assistant Hiroshi Sato. Both engineers had been in charge of aircraft design at the Aviation Research Department, Naval Technical Research Institute. The aircraft was built at the Kawasaki Dockyard, with the construction being completed in September 1928. Flight tests began in March 1929 at Kasumigaura under the control of Navy Cdr Sakae Yamamoto. However, tests were suspended after very few flights because of problems with flap operation. The flaps were considered to be a major feature of this aircraft and their use at such an early date deserves to be recorded in aeronautical engineering history. But early suspension of the tests without further refinements to the flaps, coupled with top-secret security, resulted in the lack of public awareness and has deprived this design of its rightful place in history. With this aircraft Kawasaki's affiliation with the Japanese Navy ended, and the company became solely a manufacturer of Army aircraft and a few civil types.

General characteristics
Single-engine cantilever parasol-monoplane with slotted flap system. All-metal construction with fabric covering.
Crew: two in open cockpits
Length: 10.65m (34ft 111/2in)
Span: 16.60m (54ft 51/2in)
Height: 3.18m (10ft 51/4in)
Wing area: 43.70sq m (470.3 98sq ft)
Wing loading: 41.2kg/sq m (8.41b/sq ft)
Power loading: 4kg/hp (8.81b/hp)
Empty weight: 1,200kg (2,6451b)
Gross weight: 1,800kg (3,9681b)
Powerplant: 450-600hp Mitsubishi-Hispano-Suiza twelve-cylinder vee water-cooled engine, driving a two-bladed wooden propeller.

Performance
Maximum speed: 142kt (164mph) at sea level
Service ceiling: 10,000m (32,808ft)
Endurance 3 hours
Multi-view illustration from Encyclopedia Vol.4

Tuesday, 16 September 2025

Mitsubishi Type 10 Torpedo Bomber 1MT1

An 1MT1N belonging to the Kasumigaura Kokutai as indicated by the letter "R2 on its tail.

The Type 10 Torpedo Bomber (company code: 1MT1. The number ten refers to the 10th year of the reign of Emperor Taisho, i.e. 1921) was the third* aircraft designed by former Sopwith designer Engineer Herbert Smith in Japan and was Japan's first domestically produced torpedo bomber. The first prototype was completed at the Nagoya Factory on August 9, 1922. On the same day, it was test flown by pilot William Jordan and armed with a 908  lb dummy torpedo, it successfully completed its maiden flight of approximately 30 minutes at the factory airfield. Subsequently, the second prototype was completed, and further trials were conducted at Kasumigaura Airfield in November. 
It was a fixed-landing-gear, single-engine, single-seat aircraft with a wooden frame covered in fabric. The first prototype was fitted with a 450-horsepower Napier Lion engine (hence the letter N in the 1MT1N designation), while the second aircraft was equipped with a 370-horsepower Lorraine engine (indicated by the L in the 1MT1L designation).
The first model was approximately 7 kg heavier due to the engine's weight, but its greater power enabled a maximum speed 13.5 knots faster under light load (1,605 kg) and a climb time to 3,048 meters reduced by 4 minutes and 12 seconds. Consequently, the type equipped with the Napier Lion engine (1MT1N) entered production, with 10 aircraft manufactured in fiscal year 1922 and 10 in fiscal year 1923, totaling 20 units. 
This Type 10 Torpedo Bomber was characterized by its adoption of a triplane configuration and its single-seat design, which meant it possessed absolutely no defensive armament against enemy fighters or other threats. The triplane configuration had been employed during the First World War in aircraft such as the British Sopwith Triplane fighter and the German Fokker Dr I fighter. It offered advantages in terms of reducing airframe size, improving maneuverability, and increasing payload capacity. The 1MT was adopted precisely for these advantages. It surpassed the biplane Blackburn Swift carrier-based torpedo bomber and Sopwith Cuckoo carrier-based torpedo bomber in agility and maneuverability, while its speed and climb rate exceeded those of the Type 10 Carrier Reconnaissance Plane (Mitsubishi 2MR). However, the triplane configuration also presented the problem of increased overall height. In the case of the 1MT, when loaded onto the aircraft carrier Hosho, its height proved excessive, leaving insufficient clearance beneath the hangar ceiling and causing difficulties in handling within the ship. Being single-seat and lacking machine guns was a trait shared with the imported Swift and Cuckoo, but practical trials demonstrated the necessity for defensive armament. Consequently, development of its successor, the biplane, two-seat Model 13 Carrier-based Attack Aircraft (Mitsubishi B1M), commenced urgently and the 1MT disappeared from the list of aircraft in service in 1924. 
Among the three Type 10 models designed by Engineer Smith, this was the shortest-lived. However, during its service, LTJG Kikuchi Tomozo(?), an instructor at Kasumigaura Air School, successfully ascended to an altitude of 7,620 meters in an 1MT equipped with an oxygen inhalation apparatus on July 4, 1923. This surpassed the Japanese altitude record set five days earlier by LTJG Ohashi in a Type 10 carrier fighter. Furthermore, on December 5 of the same year, this aircraft achieved the first successful aerial launch test of the 18-inch (45cm) domestically produced torpedo. This torpedo, developed at the Yokosuka Naval Arsenal based on the Type 44 45cm naval torpedo, saw its prototype completed in 1921. Following over fifty launch trials conducted by LT Akashiba and LTJG Kikuchi using the Type 10 Torpedo Bomber, it was confirmed that both the diving and running performance were significantly superior to the existing 14-inch short torpedo, leading to its adoption as the Type 44 Aerial Torpedo. It remained in service until around 1934, when it was replaced by the Type 91 Aerial Torpedo, developed from the outset as an aerial torpedo. This torpedo was transitional in nature for an air-launched type, and the 1MT itself proved short-lived. Nevertheless, its contribution in paving the way for air-launched torpedo attacks, which later achieved numerous combat successes, cannot be forgotten.

General characteristics
Single-engine triplane carrier-borne torpedo carrier. Wooden structure with fabric covering. Non-folding wings.
Crew: One pilot in open cockpit
Length: 9.779m (32ft lin)
Wingspan: 13.259m (43ft 6in)
Height: 4.457m (14ft 71/2in)
Wing area: 43sq m (462.863sq ft)
Wing loading 36.1kg/sq m (7.31b/sq ft)
Power loading 5.56kg/hp (12.21b/hp)
Empty weight: 1,370kg (3,0201b)
Gross weight: 2,500 kg (5,511 lb)
Powerplant: 1 × Napier Lion , 336 kW (450 hp)

Performance
Maximum speed: 209 km/h (130 mph, 113 kn)
Cruising speed 130 km/h (81 mph, 70 kn)
Climb to 3,050m (10,000ft) in 13min 30sec
Service ceiling: 6,000 m (19,680 ft)
Endurance 2.3 hours

Armament
1 × 457 mm (18 in), 800 kg (1,764 lb) torpedo

*The other two aircraft were the Mitsubishi 1MF carrier fighter and the Mitsubishi 2MR carrier-based reconnaissance aircraft.

Artwork by Nohara Shigeru of a Kasumigaura Kokutai 1MT1N featured in Model Art #553.

A photo of an 1MT1 without a tail marking I spotted on the net. Is it undergoing trials? Could it be the 1MT1N prototype with pilot William Jordan climbing in the cockpit and the dummy torpedo hanging on the belly? Note the two smaller oppenings under the exhausts and the bigger one behind them mirroring the port side seen in the previous photo.

On the other hand in this photo from Wiki, the cowling openings are different. Could this be one of the 1MT1L aircraft with the Napier Lion engine?

One of the 1MTs was converted into a seaplane by Ando Aeroplane Research Studio at Shin-Maiko beach, Chita Peninsula, Aichi Prefecture, in 1926 and was used as a passenger transport and pilot trainer.

In the 2015 Modelling Show in Shizuoka, I spotted a fantastic 1MT1 built by Tanaka Yoshihiro of Stall. (Marusan 1/50 kit seen below)

Tuesday, 9 September 2025

Mitsubishi A5M "Claude" by Fabio Balzano

Here's another Mitsubishi A5M in 1/72, this time a Mk.4, obtained by modifying the less-than-perfect Hobby Boss A5M2b kit. The new shape of the windscreen is a home made vacuform.
This is a very worn aircraft from the Omura Kokutai, Omura Airbase, Nagasaki Prefecture, in August 1945.
I hope you like it!

Fabio Balzano - Italy

Sunday, 7 September 2025

Mitsubishi MC-20 - video


A vintage video introducing the latest civilian transport aircraft; the Mitsubishi MC-20.
The name, MC, was inspired by the Douglas series of transports like the DC-2 and the DC-3 and it naturally meant"Mitsubishi Commercial".
It should be noted that as a name it was an one-off, i.e. there were no "MC-19" or "MC-22". The civilian version of he Mitsubishi Ki-21 "Sally" bomber is sometimes reffered to as "MC-21" but the Army was unwilling to adopt a civilian-based designation and opted, at least officially, for "M-21" instead. 
The Army version of the MC-20 was the Ki-57. More about the type, here.
Of particular interest is the overall look of the aircraft fresh out of the factory, with some parts painted gray and others seemed to be left unpainted.

Friday, 5 September 2025

Hanriot / Mitsubishi HD.14 Trainer - video


An extremely rare and surprisingly clear short clip features an Hanriot HD.14 Trainer, of which 145 were licence-built by Mitsubishi for the Imperial Japanese Army receiving the designation "Type Ki Trainer". Note the overall IJAAF "hairyokushoku" (gray green).

Friday, 15 August 2025

What-if Kyushu J7W3 "Shinden-Kai" by DizzyFugu

1:72 Kyushu J7W3 "Shinden-Kai" (A-343-)15, 343th Kokutai/301st Hikotai, Imperial Japanese Navy (IJN), piloted by CPO Yishida Masaoka; Matsuyama AB (Shikoku/Takanawa peninsula, Japan), early 1946 (Whif/modified Hasegawa kit)

Some background:
In 1943, the IJN issued an 18-shi specification that included the requirement for a new interceptor. Japanese aircraft tasked with interception roles had by this time begun to be eclipsed by the newest Allied fighters and the IJN sought to ensure their edge was main-tained. Three contenders submitted their designs, and it would be Kyushu's that was the most radical of them all: the J7W Shinden. The Kyushu J7W "Shinden" (震電, "Magnificent Lightning") was a World War II Japanese propeller-driven fighter plane with wings at the rear of the fuselage, a nose-mounted canard, and a pusher engine. Developed by the IJN as a short-range, land-based interceptor, the J7W was a response to Boeing B-29 Superfortress raids on the Japanese Home Islands. 

The man behind the "Shinden" was Captain Masaoki Tsuruno, a member of the Technical Staff of the IJN. Tsuruno conceived an interceptor that made use of a configuration rarely seen at the time of his design work, a design with canard fore planes. Canards were not a new concept, even in 1943. They were seen as far back as 1910 with a Gabriel and Charles Voisin design and later a Bleriot tail-first aircraft had incorporated canards. Tsuruno felt canards could offer a num-ber of advantages such as reducing the chances of stalling, improved controllability and maneuverability and easing some construction concerns such as the engine installation and control linkage arrangements. Tsuruno also believed the design could easily be retrofitted with a turbojet, when suitable engines became available, and the radical J7W was originally designed as a jet aircraft. At this time, the "Shinden" was known as the X-18. His ideas were worked out by the First Naval Air Technical Arsenal (Dai-Ichi Kaigun Koku Gijitsusho), which designed three gliders, designated Yokosuka MXY6, featuring canards. These were built by Chigasaki Seizo K. K., and one was later fitted with a 22 hp Semi 11 (Ha-90) 4-cylinder air-cooled engine.

By the time Tsuruno's initial layout for the "Shinden" was complete the IJN had already issued its late 1943 18-shi specifications for three classes of aircraft. The first of these covered an air superiority fighter (18-shi Ko), the second for an interceptor (18-shi Otsu) and the third for a night fighter (18-shi Hei). For the 18-shi Otsu competition, both Nakajima and Kawanishi had submitted designs: the single-engine J6K1 "Jinpu" (Squall) and the twin-engine J5N1 "Tenrai" (Heavenly Thunder) respectively. These entries were based on the rather sparse directives of the specification which called for a top speed of 665km/h (413mph), a climb to 8,000m (26,246ft) in nine minutes and the ability to carry at least two 30mm cannons. To go with these two projects, Tsuruno introduced the X-18  to the IJN as a third competitor.
The feasibility of the canard design was proven by both the powered and unpowered versions of the MXY6 by the end of 1943, and the Navy were so impressed by the flight testing, they instructed the Kyushu Aircraft Company to design a canard interceptor around Tsuruno's concept. Kyushu was chosen because both its design team and production facilities were relatively unburdened, and Tsuruno was chosen to lead a team from Dai-Ichi Kaigun Koku Gijitsusho to aid Kyushu's design works. The aircraft was officially designated J7W; in the IJN designation system, "J" referred to land-based fighters and "W" to Watanabe Tekkojo, the company that oversaw the initial design.
The construction of the first two prototypes started in earnest by June 1944, stress calculations were finished by January 1945, and the first prototype was completed in April 1945. The "Shinden" would carry four Type 5 30mm cannons. The Type 5, while heavier than the earlier Type 2 30mm gun, possessed a higher rate of fire at 500 rounds per minute and had a higher muzzle velocity. Each cannon was provided with 66 rounds. With less than eight seconds of 30mm rounds per gun, one hit would be sufficient to cripple and shoot down a fighter or bomber, therefore there was little ammunition to waste. Therefore, there were two Type 1 7.92mm machine guns, one on either side of the gun camera, in front of the nose. The purpose of these guns was not offensive but to serve as a ranging weapon for the cannons. Upon lining of his target, the pilot would fire a short burst from the machine guns. If the rounds struck the target, he would fire a burst from the cannons and be reasonably assured of a hit, thereby conserving the precious cannon ammunition. Each Type 1 was provided with 75 rounds of ammunition in a saddle drum magazine. For payload, the "Shinden" had a modest bomb carrying capacity of 120kg (264 lb).
The 2,130 hp Mitsubishi MK9D (Ha-43) radial engine and its supercharger were installed behind the cockpit and drove a six-bladed propeller via an extension shaft. Engine cooling was to be provided by long, narrow, obliquely mounted intakes on the side of the fuselage. It was this configuration that caused cooling problems while running the engine while it was still on the ground. This, together with the unavailability of some equipment parts, postponed the first flight of the "Shinden". The aircraft turned out to be agile but not easy to fly. The "Shinden" was found to have a relatively fast landing speed at 240km/h (149mph), its massive propeller and extension shaft caused substantial torque pull to the right and the aircraft had the unpleasant tendency to drop its nose at any speed. Especially bringing the "Shinden" down safely was not a simple task.

However, even before the "Shinden" took flight the IJN was desperately in need of a high-performance interceptor. The Kawanishi J6K1 "Jinpu" failed to show any improvement over the Kawanishi N1K2-J "Shiden-Kai" (meaning 'Violet Lightning', known to the Allies as George) and the Nakajima J5N1 "Tenrai" was proving to be a disappointment by the time flight trials commenced in July 1944. With the failure of these two entries for the 18-shi specification, the IJN ordered the J7W1 "Shinden" into production in May 1944 and in so doing made the type the only canard configuration aircraft to achieve this status during World War 2. By September 1944, the production plans had been formulated with Kyushu's Zashonokuma factory expected to turn out 30 "Shindens" per month while Nakajima's Handa plant would produce 120 "Shindens" each month. While serial production was ramped up, work on the J7W airframe continued: the propeller-driven aircraft were soon improved to get rid of the handling issues: the front canards were placed at 7.5° positive incidence, the center of gravity was adjusted and the extension shaft for the propeller pointed 3° to the right and 4.5° down from the zero thrust line.

In parallel, work on a more potent jet-powered version, as originally envisioned, continued, the  J7W2 "Shinden-Kai". This was to be the turbojet-equipped version of the "Shinden". The already available Ne 12B engine was rejected as its power was considered too low to effectively propel the aircraft. In any case, work was by this time under way on the Kugisho Ne 20 turbojet that was based on the German BMW 003A engine, the only turbojet built and flown in a Japanese aircraft so far: the Nakajima "Kikka". Two of these engines were proposed to power the J7W2 but mounting them required a substantial redesign of the rear hull. A J7W2 prototype had been converted from a J7W airframe by April 1945, but it soon became clear that the aircraft was underpowered - it never got from the ground and only made high-speed taxiing tests, before it was destroyed in a bomb raid. However, the aircraft provided some valuable information to refine a jet-powered version of the "Shinden". For instance, the original narrow air intake slits turned out to be ineffective, and the canards had to be enlarged to improve balance and control.

Another variant of the "Shinden-Kai" was the J7W3, and this aircraft was to use the Ne 130 turbojet, also based on the BMW 003A, which was being developed by Ishikawajima-Shibaura. The Ne 130 was to have produced nearly double the thrust of the Ne 20, and this promised to be sufficient to exceed the propeller-driven J7W's performance and warrant further development. Together with the data gathered from the J7W2 the resulting aircraft retained the "Shinden's" core airframe but underwent considerable detail modifications. The most obvious difference were new air intakes on the wing roots, leading in constant diameter ducts to the engines that were now housed in more organic and aerodynamically more efficient nacelles that ran along the fuselage flanks. The tail section was also extended, ending now in a pen nib fairing that moved the center of gravity further back and improved aerodynamics. The canards and therewith wing area was increased. To save internal space the landing gear was shortened, resulting in smaller wells. The freed space was used for two additional 125 l wing tanks and an increased ammunition load of 90 30 mm rounds per gun. Due to the expected high speed and frontline experience with the J7W's arrangement, the two Type 1 7.92mm machine guns were deleted. Since the landing gear was shorter and there was no propeller anymore to protect, the twin fins' shape was also changed: they became taller while the lower halves were reduced in size, and their overall area was slightly increased to improve longitudinal stability. Most of the wings and the hull remained untouched, even though the different engine arrangement allowed an additional 450 l tank in the fuselage behind the cockpit, which remained unmodified, too. 

By the time the J7W3 entered hardware stage its intended powerplant also had made progress: this became the Ne 130-II, an improved design that was more reliable and produced 10.76 kN (2,420 lbf) / 10,000 rpm / sea level. Its weight was only 649 kg, and it featured one extra compressor and turbine stage for higher thrust, only lengthening the engine by 303 mm (11+15⁄16 in) overall compared to the original Ne 130. With these more advanced engines the J7W3 became a fighter to be reckoned with, offering a performance comparable with the German Messerschmitt Me 262 twin jet fighter. 
However, in dire need for an interceptor that could cope with the incoming American high-flying B-29 bombers, the IJN repeated the J7W’s hasty decision and ordered the J7W3 into production even before the first prototype took to the air in July 1945, and a quota of twenty "Shinden-Kai" a month was given to Kyushu's Zashonokuma factory, while 120 J7Ws from Nakajima's Handa plant were to be produced until production was supposed to fully switch to the J7W3 towards 1946. It was estimated some 1,086 "Shinden" could be produced in total between April 1946 and March 1947.

General characteristics:
    Crew: 1
    Length: 10,80 m (35 ft 4 1/2 in)
    Wingspan: 11.11 m (36 ft 6 in)
    Height: 3.42 m (11 ft 2 1/2 in)
    Wing area: 21.8 m² (234 sq ft)
    Empty weight: 3,795 kg (8,367 lb)
    Gross weight: 6,473 kg (14,271 lb)
    Max takeoff weight: 7,130 kg (15,719 lb)   
Powerplant: 2× Ishikawajima Ne 130-II axial-flow turbojets, developing 1,100 kg (2,400 lb) of thrust each.
Performance:
    Maximum speed: 900 km/h (560 mph, 490 kn)
    Range: 1,050 km (650 mi, 570 nmi)
    Service ceiling: 11,450 m (37,570 ft)
    Rate of climb: 20 m/s (3,900 ft/min) at max weight of 7,130 kg (15,720 lb)
    Wing loading: 300 kg/m2 (61 lb/sq ft)
    Thrust/weight: 0.31
Armament:
    4× 30 mm (1.181 in) Type 5 cannon with 90 RPG 
Underwing hardpoints for 4× 30kg (66lb) or 4× 60kg (130lb) bombs or 2x 125l drop tanks

The kit and its assembly:
This fictional what-if project is a personal but somewhat history-based interpretation of what could have been, inspired by the J7W2 model/conversion that Hasegawa offers for its propeller-driven J7W "Shinden" kit, turning the latter (outwardly) into a jet-powered version. As mentioned in the background above, the J7W was originally envisioned as a jet-powered interceptor, but at a time when no suitable engine was available or even on Japanese drawing boards yet. So, it was – as an interim solution – modified to accept a radial engine with a pusher propeller, but with the perspective to switch again to a jet powerplant later. Over time the Ne-20 jet engine was developed, which was a simplified adaptation of the German BMW 003 – an axial design and rather slim. But it was experimental at best and not very powerful or reliable. It was used and flown on the Nakajima J9N "Kikka", though, but even with two of these engines the aircraft was rather underpowered and far from an effective fighter airplane, let alone a fast interceptor .
When you then take a look at Hasegawa’s conversion offer (which only consists of a different end plate with a nozzle cone instead of the prop) for a J7W2 jet version of the Shinden, it’s IMHO BS because 
a) a single indigenous jet engine like the Ne-20 and even its more powerful derivatives would never have had enough power to let the J7W airframe perform like an interceptor, let alone fly at all, and 
b) the potential engine size/shape, which would rather reflect a centrifugal engine with a much bigger diameter. The shape and size of the air intakes would also leave some doubts. 
Another factor that speaks against the Hasegawa “proposal” is the fact that there was and is apparently no reliable design sketch or layout for a re-jet-engined "Shinden".
This would not stop an ambitious model kit builder to try a personal interpretation, and effectively one that is more plausible than Hasegawa’s own rather lazy attempt. This eventually led to “my” J7W3, which took some inspiration from the very good and exhaustive description of the J7W in Edwin D. Myer’s book “Japanese Secret Projects (1)”. It discusses the potential engine options – which were all axial flow powerplants – and also suggests that there would have been some considerable hardware changes to the J7W airframe, like a modified tail section, a lowered/simplified landing gear, and therewith also different fins.
The basis became a standard Hasegawa J7W – and I had actually procured resin copies of the company’s own J7W2 conversion parts. However, I made considerable conceptual changes. The central difference was the decision to mount a pair of axial flow engines in the real hull, and I had resin upgrade parts for the twin J47 gondolas’ rear end for Hasegawa’s 1:72 B-47 kit in The Stash™. One of these was implanted into the J7W's slightly shortened tail/engine bay, adding length so that the aircraft’s center of gravity might be kept. Being much wider and flatter than the original radial engine I decided to add bigger air intakes, too, and to delete the original “slits” behind the cockpit. These were sanded away and replaced with the intakes from an Italeri BAe Hawk trainer, mounted relatively low in front of the wing’s leading edge. They look a bit modern (esp. because of their boundary layer gaps to the fuselage) but were simply perfect in size and shape. The ducts connecting the new intakes and the side-by-side engines were then sculpted with 2C putty and PSRed into the rest of the hull.
The cockpit was taken OOB, but I decided to modify the canards and give them more shape. I initially experimented with swept surfaces, but that did not look plausible and so I “just” mounted elevators from an Intech P-51 kit. Another mod was made to the landing gear: while the OOB struts and wheels were used, all parts were shortened and the respective wells were reduced in length/size accordingly, what moved the front leg forward and the main landing gear inwards, reducing track width. With less ground clearance and for a different look I also replaced the fins on the wings’ trailing edge – not an easy task, but I eventually found a pair of vintage elevators from an Airfix 1:72 F-86D kit, which were slightly modified and now occupy the original fins’ places. They are taller now, have less depth, and the lower section under the wings was dramatically shortened, too. That shape was inspired by an illustration in Edwin D. Myer’s book, and it looks quite plausible.

Another small mod was the replacement of the molded gun barrels with bits from hollow steel needles.

Painting and markings: 
I considered a lot of potential options, including a bare metal finish, an improvised camouflage over that, or even highly exotic or speculative schemes (e.g. in all-over IJN grey-green or a very pale grey). In the end I settled for a simple/conservative IJN green/grey livery for land-based aircraft. Boring, yes, but the aircraft itself was already so exotic that I wanted to keep the looks more standard, and therewith more convincing.
However, I built the paint up so that aluminum would shine through here and there, and I painted upper surface areas in different shades of dark green (including ModelMaster’s IJN Dark Green and Humbrol 2, 195 and 239). The underside was painted with Humbrol 40 (Light Gull Grey), and the low waterline became quite wavy.
The cockpit tub was painted in a yellowish green (a mix of Humbrol 63 and 226) while the landing gear wells were initially painted with aluminum and received a coat with translucent bright blue lacquer, simulating aodake iro. The landing gear struts became glossy black.

The model received a light black ink washing, thorough post-panel shading in various mixed shades of dark green on the upper surfaces, plus dry-brushing with silver to simulate flakes paint here and there. The exhaust fairings were painted with Revell 91 (Iron metallic) and treated with graphite to provide them with an uneven and more metallic/burnt shine. 

Markings came mostly from a PrintScale Kawanishi N1K kit, with typical late-war IJN markings. The yellow ID bands on the wings' leading edges were created with generic decal material (TL Modellbau) instead of trying to mask and paint them. Stencils were mostly taken from the Hasegawa J7W's OOB sheet. Finally, the model was sealed with a sheen acrylic varnish (a mix of semi-gloss and matt Italeri varnish) and the wire antenna, made from black heated sprue material, was added.
A project that I had had on my agenda for a long time, and I am happy that I eventually tackled it – and it turned out better and more plausible than expected! Despite the hand-sculpted air ducts/engine fairings the aircraft’s outlines do not look too fantastic, and the new tail section makes the "Shinden" look pretty fast, if not elegant. The shorter landing gear also suits the aircraft well, and I think that sticking to the classic green/grey IJN livery was the right move, because it suits the "Shinden" well and just underlines its “serious” origins as a real but undocumented development project.