Kawasaki Ki-148
| Ki-148 | |
|---|---|
| Type | Guided air-to-surface missile |
| Place of origin | Japan |
| Production history | |
| Manufacturer | Kawasaki Kōkūki Kōgyō K.K. |
| Produced | 1944-1945 |
| No. built | ~180 |
| Specifications | |
| Mass | 680 kg (1,500 lb) |
| Length | 4.09 m (13 ft 5 in) |
| Warhead | HEAT |
| Warhead weight | 300 kg (661 lb) |
| Wingspan | 2.6 m (8 ft 6 in) / Wing area: 1.95 m2 (21 sq ft) |
| Propellant | 1 x 1.47 kN (330 lbf) thrust |
Guidance system | radio-control |
Launch platform | Kawasaki Ki-102 in service (Kawasaki Ki-48 for trials) |
| References | Japanese Aircraft of the Pacific War[1] |
Kawasaki Igo-1-B, otherwise known as Kawasaki Ki-148 was a World War II Japanese guided air-to-surface missile designed in 1944. Developed along its sister projects of and Tokyo Imperial University designed , the Igo-1-B was a simple radio-controlled guided bomb propelled by a rocket engine generating 1.47 kN (330 lbf) of thrust for up to 80 seconds.[2]
Test trials were carried out in late 1944 and the weapon was quickly ordered by the war ministry. Launched during tests from a modified Kawasaki Ki-48 light bomber, its standard was to be the modern Kawasaki Ki-102 heavy fighter. Although approximately 180 missiles were built, none saw service before the end of World War II.[1]
References[]
- ^ a b Francillon 1979, p. 532.
- ^ Martin Caidin (1956). "Japanese Guided Missiles in World War II". Journal of Jet Propulsion. 26 (8): 691–694.
- Bibliography
- Francillon, René J. Ph.D. (1979). Japanese aircraft of the Pacific War (2nd ed.). London: Putnam. p. 532. ISBN 0-370-30251-6.
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