From Wikipedia, the free encyclopedia.
| Mitsubishi Ki-202 | |||
|---|---|---|---|
 | |||
| Description | |||
| Role | Interceptor | ||
| Crew | one, pilot | ||
| Dimensions as designed | |||
| Length | 7.10m | 23' 3" | |
| Wingspan | 9.75m | 32 | |
| Height | 2.70m | 8' 10" | |
| Wing area | 18.4m² | 198 ft² | |
| Weights as designed | |||
| Empty | |||
| Loaded | 5,100kg | 11,220 lb | |
| Powerplant | |||
| Engine | 1x Toko Ro.3 rocket | ||
| Power | 19.6kN | 4,400 lb | |
| Performance anticipated | |||
| Maximum speed | 900km/h | 560 mph | |
| Endurance | |||
| Service ceiling | |||
| Rate of Climb | |||
| Armament | |||
| Guns | 2x 30mm Ho-105 cannons | ||
The Mitsubishi Ki-202 Shusui-Kai (Japanese: 三菱 Ki-202 秋水改, "Shusui-Kai" translated as "Swinging Sword, Improved", or "Sword-stroke, Improved") was a development of the Mitsubishi J8M rocket-powered interceptor aircraft, based in turn on the German Messerschmitt Me 163. None were produced before Japan's surrender that ended World War II.
A fundamental shortcoming of the Me 163 and all other aircraft based on it was extremely limited endurance, typically only a few minutes. The Imperial Japanese Navy proposed to improve the endurance of the J8M1 by producing a version with only one cannon, thereby saving weight and space for more fuel (J8M2). The Army, on the other hand, opted to keep both cannons but enlarge the airframe to accommodate larger tanks.
This aircraft, the Ki-202 was to have been the definitive Army version of the fighter. To further save fuel, the aircraft was to have been launched by catapult.
