“Kawasaki Ki-148”的意思、由来-开放百科全书

词条

Kawasaki Ki-148

释义

Specifications
References

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 Mitsubishi Igo-1-A and Tokyo Imperial University-designed Igo-1-C, the Igo-1-B was a simple radio-controlled guided bomb propelled by a rocket engine generating {{convert|150|kg|lb}} of thrust for up to 80 seconds.^[1]

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 mother aircraft 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.^[2]

Specifications

Length: {{convert|4.09|m|ftin|abbr=on}}
Wing Span: {{convert|2.60|m|ftin|abbr=on}}
Height: {{convert|0.90|m|ftin|abbr=on}}
Wing Area: 1.95 Square metres
All-Up Weight: 680 kg
Main Engine: 1 x Mitsubishi Tokuro-1 Type 2 Rocket (150 kg)
Max Speed: unknown
Range: unknown
Warhead: 300 kg HEAT

References

Notes

1. ^{{Cite journal|author=Martin Caidin | author2= |title=Japanese Guided Missiles in World War II | publisher= |journal=Journal of Jet Propulsion|asin= |volume=26 |issue=8 | date=1956 |pages=691–694 |url=http://arc.aiaa.org/doi/abs/10.2514/8.7117?journalCode=jjp}}
2. ^{{Harvnb|Francillon|1979|p=532.}}

Bibliography

Francillon, Ph.D., René J. Japanese Aircraft of the Pacific War. London: Putnam and Company Ltd., 1979. {{ISBN|0-370-30251-6}}.

4 : Kawasaki aircraft|Air-to-surface missiles|World War II weapons of Japan|World War II guided missiles

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