Arawasi Japanese Aviation History

Aichi B7A1 "Ryusei" (Grace) by Jan VoorbijAichi B7A1 "Ryusei" (Grace)Dive bomber / TorpedobomberPre-production plane: 1 ...
20/09/2025

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

"Hayabusa Fighter Group" by DNKThe fifth book in the IJAAF Unit series by Dainippon Kaiga is dedicated to the 50th Senta...
19/09/2025

"Hayabusa Fighter Group" by DNK

The fifth book in the IJAAF Unit series by Dainippon Kaiga is dedicated to the 50th Sentai, based on the photos in the Kikuchi Collection. There are 2 pages of excellent artwork by Sato Kunihiko with various "Hayabusa" details, 6 pages of artwork by Yoshino Yasutaka of side profiles showing the details of the paint schemes, 7 pages with color photos of the restored "Hayabusa" in the FHCAM, 61 pages with 52 b/w photos from the Kikuchi collection and about 15 pages with a rough history of the unit and other information.
All the text is in Japanese with no English translation.
Not the best release by DNK but an interesting publication nonetheless.

Title: "Hayabusa Fighter Group" (The Pictorial Brief History of the 50th Sentai)
Authors: various
Pages: 96
Size: 20X25cm
Published by: Dainippon Kaiga, Sept. 2019

Price: $US 22.00 (Postage NOT included)
Send over a PM or email us if interested with your name and delivery address (to calculate postage): [email protected]

18/09/2025

Nakajima Ki-43 "Hayabusa" (Oscar), "Tsubasa no Gaika" 一式戦闘機「隼」, 翼の凱歌 - video

A clip today from the movie "Tsubasa no Gaika" featuring a Nakajima Ki-43 "Hayabusa" with Okawa Takashi, played by actor Tsukita Ichiro* "in the cockpit"**. An absolute pleasure to see a "Hayabusa" doing all these aerobatics!
A shortened version of the clip has appeared on various FB pages without the original sound or any credit. The info below is from the Japanese Wiki:

『Tsubasa no Gaika』 (The Triumph of Wings) is a war film produced by Toho and released on 15 October 1942.
Synopsis
Two boys, orphaned at a young age when their father—a pilot and aviation engineer—perished in a storm during a crash, were raised as foster brothers by the wife of the crashed pilot. The elder brother aspired to become a juvenile air cadet and rose to become an ace pilot (fighter pilot) in the Imperial Japanese Army Air Force. The younger brother, after training at an aircrew training school, developed into a test pilot for the Nakajima Aircraft Company's Ki-43 (later the Type 1 Fighter "Hayabusa") at Nakajima Aircraft, growing into test pilot who excel both in development and on the battlefield.
The narrative weaves in the untold story of developing the Army's primary fighter of the era. By featuring stepbrothers who pursue distinct paths – one as an Army pilot, the other as a civilian pilot – it crafts a success story depicting their growth: one as a frontline soldier, the other as a civilian on the home front. Furthermore, by introducing a widow who watches over the two men, it illustrates the mindset of the beautiful Yamato Nadeshiko, the quintessential Japanese woman, during wartime ( https://en.wikipedia.org/wiki/Yamato_nadeshiko ).
The film was sponsored by the Army Air Headquarters. All aircraft used in filming were actual aircraft, with the exception of some special effects scenes. Furthermore, the aircraft's details, such as the sighting device and oil cooler, scenes from engine start-up through take-off to landing, and aerobatic flight, are depicted with remarkable clarity. The "Hayabusa", arguably the third protagonist, is filmed extensively and without omission over a long duration, making this work akin to a promotional video for the "Hayabusa". In this respect, it stands alongside the 1940 film “Burning Skies” and the 1944 film “Kato's Hayabusa Fighter Squadron” – both of which also utilised real aircraft extensively for filming – as an extremely valuable visual historical document.
Furthermore, the screenplay was co-written by Akira Kurosawa, who would later become a world-renowned director, and Bōhei Toyama. The special effects scenes, like those in contemporary war films such as The Battle of Hawaii-Malay and The Kato Hayabusa Combat Squadron, were handled by Eiji Tsuburaya ( https://en.wikipedia.org/wiki/Eiji_Tsuburaya ). However, due to the cooperation of the Army, many scenes featured actual aircraft, meaning the special effects scenes were limited to crashes and shoot-downs.

Director: Yamamoto Satsuo
Screenplay: Toyama Bonpei, Kurosawa Akira
Cast: Oka Jōji, Tsukita Ichirō, Irie Takako
Music: Hattori Ryōichi
Cinematography: Kanakura Taiichi
Production Company: Toho Film
Released 15 October 1942
Running time 109 minutes

The dialogue between the pilot and ground crew members goes like this:
GC1: Hatsudoki no choshi was do desh*ta
(How was the engine?)
P: Aa, ii yo
(Oh, it was fine)
GC1: Ah so desu ka
(Oh, really!)
GC2: Dodai guwai wa?
(How do you feel?)
P: Kesaku da yo
(Great!)
PC2: Kaji no kiki wa?
(How about the controls?)
P: Mmm, ii, shikashi teppo tsunde minai to wakaran na, ima wa sukoshi karui kara
(Hmmm, good but I'm not sure without having the guns installed, 'cause it's a bit light now)
GC2: Sore mo so da. Shindo wa?
(That's right. Any vibration?)
P: Daijobu da
(It's okay)
GC2: Hatsudoki no kaiten wa
(how is the engine behaving?)
P: Yoku wo ieba, sukoshi tarinai kimo suru kedo, ma tonikaku kesaku dayo. Hisashiburi ni omou zombun tonde mita yo!
(If I'm being picky, it feels a tad underpowered, but it's a masterpiece nonetheless. It's been ages since I've flown to my heart's content!)

*Shortly after the end of the war, on 27 September 1945, he died from methanol poisoning. He was only 35 years old.
**At 00:47 and 02:35 he is actually sitting in the rear cockpit of a Tachikawa Ki-55 trainer. But from 04:21 he is indeed bringing the plane to a standstill on his own!!!

Mitsubishi A5M "Claude" by Fabio BalzanoHere's another Mitsubishi A5M in 1/72, this time a Mk.4, obtained by modifying t...
16/09/2025

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

"The Imperial Japanese Navy Interceptor Shiden N1K1-J series"A DNK publication dedicated mostly to the Kawanishi N1K1-J ...
15/09/2025

"The Imperial Japanese Navy Interceptor Shiden N1K1-J series"

A DNK publication dedicated mostly to the Kawanishi N1K1-J "Shiden" prototype. Dozens of high-quality photos appear first time in print covering every detail of the prototype. There are seven pages with color illustrations by artist Sato Kunihiko (from Model Art) as well as side and bottom color views by Yoshino Yasutaka of "Shiden" belonging to various units. There is also a chapter with a few photos and drawings detailing the various differences between the "Shiden" prototypes, pre-production and production versions. Unfortunately NO ENGLISH in the book but a highly recommended one nonetheless.

Title: "The Imperial Japanese Navy Interceptor Shiden N1K1-J series - photo & illustlated (sic)"
Authors: Yoshino Yasutaka
Published by: Dainippon Kaiga, Feb. 2017.
Pages: 127
Photos: 144
Profiles: 13
Size: 21X26cm

Price: $US 29.00 (Postage NOT included)
Send over a PM or email us if interested with your name and delivery address (to calculate postage): [email protected]

Kawasaki Ki-48 "Lily" and "Ne0" 九九式双発軽爆撃機とネ0ラムジェットエンジンAs the Second World War intensified, the front lines demanded high...
14/09/2025

Kawasaki Ki-48 "Lily" and "Ne0" 九九式双発軽爆撃機とネ0ラムジェットエンジン

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. Two-stage axial-flow motor jet ‘Ne1’, single-stage centrifugal motor jet ‘Ne2’, three-stage axial-flow turbojet ‘Ne3’, single-stage centrifugal turbojet ‘Ne4’, and the ramjet ‘Ne0’ for fundamental research.
The Ne-1 and Ne-2 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 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 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.
Ne-0 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.

Kobeseiko "Te-Go" Experimental Observation AircraftDesigned by Professor Miki Tetsuo of the Department of Aeronautics, F...
13/09/2025

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)

Mitsubishi Army Experimental "Tobi" Reconnaissance Aircraft (Company designation 2MR1)In 1926, the IJAAF sought competit...
12/09/2025

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 https://en.wikipedia.org/wiki/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.

Experimental 7-Shi Carrier Attack Aircraft (Nakajima B4N1, Y3B)In April 1932, the Navy issued instructions to Mitsubishi...
11/09/2025

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: http://hsfeatures.com/features04/b4n1fm_1.htm

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...

Nakajima Bulldog FighterNakajima's design for a parasol-wing fighter, along with those of other companies competing for ...
10/09/2025

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 assist-ant 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 of four variants, 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 Chikuhei Nakajima 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)

Kawasaki Experimental Carrier Reconnaissance Aircraft In March 1927, the Navy decided to manufacture an experimental air...
09/09/2025

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

Mitsubishi 1MT1 十年式艦上雷撃機The Type 10 Torpedo Bomber (company code: 1MT1. The number ten refers to the 10th year of the re...
08/09/2025

Mitsubishi 1MT1 十年式艦上雷撃機

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 ( https://en.wikipedia.org/wiki/Herbert_Smith_(aircraft_designer) ) 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.

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1-32-1, #701 Kizawa
Toda-shi, Saitama

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