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Mitsubishi J8M / Ki-200 Shūsui

The Mitsubishi J8M Shūsui, was a Japanese World War II rocket-powered interceptor aircraft closely based on the German Messerschmitt Me 163 Komet.

The J8M1 was intended to be a licence-built copy of the Messerschmitt Me 163 Komet.

Difficulties in shipping an example to Japan meant that the aircraft eventually had to be reverse engineered from a flight operations manual and other limited documentation.

A single prototype was tested before the end of World War II.

The Japanese were aware of the results of the strategic bombing of Germany and knew that the B-29 Superfortress would be bombing Japan and the resultant problems which would arise from trying to combat this.

Japanese military attachés had become aware of the Komet during a visit to the Bad Zwischenahn airfield of Erprobungskommando 16, the Luftwaffe evaluation squadron charged with service test of the revolutionary rocket-propelled interceptor.

They negotiated the rights to licence-produce the aircraft and its Walter HWK 509A rocket engine.

The engine licence alone cost the Japanese 20 million Reichsmarks (equivalent to 81 million 2021 euros).

The broken-down aircraft and engine were sent to Kobe, Japan in early 1944.

It is probable that the airframe was on the Japanese submarine RO-501 (ex-U-1204), which left Kiel, Germany on 30 March 1944 and was sunk in the mid-Atlantic on 13 May 1944 by the hunter-killer group based on the escort carrier USS Bogue.

Plans and engines were on the Japanese submarine I-29, which left Lorient, France on 16 April 1944 and arrived in Singapore on 14 July 1944, later sunk by the submarine USS Sawfish on 26 July 1944, near the Philippines, after leaving Singapore.

The Japanese decided to attempt to copy the Me 163 using a basic instructional manual on the Komet in the hands of naval mission member Commander Eiichi Iwaya who had travelled to Singapore in the I-29 and flown on to Japan when the submarine docked.

From its inception, the project was a joint Imperial Japanese Army Air Service (JAAF)/Imperial Japanese Navy Air Service (JNAF) venture.

The JAAF wanted a new design to be drawn up.

The JNAF, on the other hand, felt the design should mimic the German Komet because it had already proven to be a stable aerodynamic body.

It was the JNAF which won and issued the 19-shi specification in July 1944 for the design of the rocket-powered defence fighter.

The contract went to Mitsubishi Jukogyo KK, which would produce both the JNAF version the J8M1 Shūsui and the JAAF version Ki-200.

The project was headed by Mijiro Takahashi.

The JAAF, however decided to undertake their own design to meet the 19-shi specifications, working at their Rikugun Kokugijitsu Kenkyujo (JAAF Aerotechnical Institute) in secret.

At the 1st Naval Air Technical Arsenal in Yokosuka, in association with Mitsubishi and Yokosuka Arsenal, work began to adapt the Walter HWK 509A engine to Japanese manufacturing capabilities and techniques.

This was also where efforts were underway to produce a glider version of the J8M to provide handling data.

While working on this glider, the MXY8 Akigusa, Mitsubishi completed a mock-up of the J8M1 in September 1944.

Both the JAAF and JNAF approved its design and construction, and a prototype was built.

In December 1944, the MXY8 was completed and, on 8 December 1944, at the Hyakurigahara Airfield, Lieutenant-Commander Toyohiko Inuzuka took the controls of the MXY8.

Once in the air, Inuzuka found the MXY8 almost perfectly emulated the handling characteristics of the Komet.

Two additional MXY8 gliders were constructed in the naval yard at Yokosuka, one being delivered to the Rikugun Kokugijitsu Kenkyujo (JAAF Aerotechnical Institute) at Tachikawa for evaluation. The JNAF initiated the construction of another prototype, production designation Ku-13.

This was to use water ballast to simulate the weight of an operational J8M complete with engine and weapons.

This variant was to be built by Maeda Aircraft Institute, while the JAAF version was to be constructed by Yokoi Koku KK (Yoki Aircraft Co).

The JNAF also proposed a more advanced trainer, designated the MXY9 Shūka (秋火, “Autumn Fire”) which would be powered by a 2 kN (450 lbf) thrust Tsu-11 ducted-fan engine.

The war, however, ended before this model could be built.

Mitsubishi and partners Nissan and Fuji proceeded with development of the airframe and Yokosuka Arsenal was adapting the engine for Japanese production, designated the Ro.2.

The Japanese succeeded in producing prototypes that outwardly looked very much similar to the Komet.

The J8M1 had a wet weight that was 400 kg (880 lb) lighter, the aircraft having a plywood main spar and wooden vertical tail.

The designers had also dispensed with the armoured glass in the cockpit and the aircraft carried less ammunition and slightly less fuel.

The Ki-200 and the J8M1 differed only in minor items, but the most obvious difference was the JAAF’s Ki-200 was armed with two 30 mm (1.18 in) Type 5 cannon (with a rate of fire of 450 rounds per minute and a muzzle velocity of 720 m/s (2,400 ft/s)), while the J8M1 was armed with two 30 mm (1.18 in) Ho-105 cannon (rate of fire 400 rounds per minute, muzzle velocity 750 m/s (2,500 ft/s).

The Ho-105 was the lighter of the two and both offered a higher velocity than the MK 108 cannon of the Me 163 (whose muzzle velocity was 520 m/s (1,700 ft/s).

The Toko Ro.2 (KR10) rocket motor did not offer the same thrust rating as the original, and Mitsubishi calculated that the lighter weight of the J8M1 would not offset this.

Performance would not be as good as that of the Komet, but was still substantial.

The engine used the German propellants of T-Stoff oxidizer and C-Stoff fuel (hydrogen peroxide/methanol-hydrazine), known in Japan as Ko and Otsu respectively.

A total of 60 of the training versions (Ku-13, Ki-13, MXY-8, MXY-9) were produced by Yokosuka, Yokoi and Maeda.

Seven of the operational versions (J8M1/Ki-200) were built by Mitsubishi.



An interceptor variant for the IJAAS, almost identical to the IJNAS J8M


Rocket-powered interceptor aircraft closely based on the German Messerschmitt Me 163 Komet.

J8M2 Shūsui Model 21

Long-range version for Navy, identical to J8M1, but armament reduced to a single 30 mm (1.18 in) cannon.

J8M3 Shūsui Model 22  / Rikugun Ki-202 Shūsui-kai

Long-range version for Army and Navy, with fuselage and wingspan lengthened to 7.10 m (23 ft 3 in) and 9.75 m (32 ft 0 in) respectively, powered by 19.6 kN (4,410 lbf) Tokuro-3, projected maximum speed 900 km/h (560 mph).

Yokosuka MXY-8 Akigusa / Yokoi Ku-13

Training glider using J8M air frame for Navy and Army.

Yokosuka MXY-9 Shuka

Training version using J8M airframe, powered by Tsu-11 Thermojet engine.


J8M1 / J8M2 / Ki-200




9.50 m (31 ft) 9.47 m (31 ft)


6.03 m (20 ft) 5.88 m (19 ft)


2.68 m (9 ft) 2.68 m (9 ft)

Wing area 

17.72 m2 (191 sq ft) 17.69 m2 (190 sq ft)

Wing loading 

219.22 kg/m2 (44.9 lb/ft2) 219.70 kg/m2 (45 lb/ft2) 

Empty weight 

1,445 kg (3,186 lb) 1,510 kg (3,329 lb) 1,505 kg (3,318 lb)


3,000 kg (6,614 lb) 3,650 kg (8,047 lb)


3,870 kg (8,532 lb) 3,900 kg (8,598 lb) 3,870 kg (8,532 lb)

Useful load 

1,545 kg (3,406 lb) 2,140 kg (4,718 lb)     

Fuel capacity 

T-Stoff = 1,181 l (260 imp gal)

C-Stoff = 522 l (115 imp gal)



2x Type 5 30mm cannon, 2x Type 5 30mm cannon, 2x Ho-155 30mm cannon or 2x Ho-5 20mm cannon


53 rounds per gun



One Toku-Ro.2 (KR10) bi-fuel rocket motor developing 1,500 kg (3,307 lb) of thrust.


T-Stoff = 80% Hydrogen Peroxide + 20% Oxyquinoline and Pyrophosphates

C-Stoff = 30% Hydrazine Hydrate + 70% Methanol, Water and Potassium – Copper Cyanides

Max speed

900 km/h (559 mph) at 10,000 m (32,808 ft)

Cruise speed 

699 km/h (434 mph) 351 km/h (218 mph)

Landing speed 

150 km/h (93 mph)            


3 min 06 seconds of powered flight, 2 min 30 seconds of powered flight

Max range 

5 min 30 seconds of powered flight, 7 min of powered flight.


2,000 m (6,562 ft) in 40 seconds

4,000 m (13,123 ft) in 2 minutes 08 seconds

8,000 m (26,247 ft) in 3 minutes 08 seconds

10,000 m (32,808 ft) in 3 minutes 50 seconds               

10,000 m (32,808 ft) in 3 minutes 40 seconds

Rate of climb 

43.47 m/s (8,557 ft/min), 45.45 m/s (8,947 ft/min)


12,000 m (39,370 ft).



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