Saturday, 20 September 2025
Aichi B7A1 "Ryusei" (Grace) by Jan Voorbij
Thursday, 18 September 2025
Kawasaki Experimental Carrier Reconnaissance Aircraft
Tuesday, 16 September 2025
Mitsubishi Type 10 Torpedo Bomber 1MT1
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)
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
1 × 457 mm (18 in), 800 kg (1,764 lb) torpedo
Tuesday, 9 September 2025
Mitsubishi A5M "Claude" by Fabio Balzano
Sunday, 7 September 2025
Mitsubishi MC-20 - video
Friday, 5 September 2025
Hanriot / Mitsubishi HD.14 Trainer - video
Friday, 15 August 2025
What-if Kyushu J7W3 "Shinden-Kai" by DizzyFugu
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.
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.
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.
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
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 .
Another small mod was the replacement of the molded gun barrels with bits from hollow steel needles.
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.