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.