Japan's Mitsubishi F1M reconnaissance floatplane, Navy Type 0
Allied Code Name: Pete
Design
The Mitsubishi F1M was designed to be a catapult launched observation floatplane.1 It was to meet a late 1934 Imperial Japanese Navy specification for a replacement for the Nakajima E8N1.1,2 Aichi and Kawanishi also tried to meet the requirements.2 Kawanishi withdrew and Aichi's was inadequate.2
The Mitsubishi design team was lead by Joji Hattori.2
A couple problems the F1M had was it would often porpoise in water and directional stability in flight.1
Floats
There was a main, central, float, and two stabilizers attached to the lower wing.2
Upgrade
The F1M2 was a major redesign that appeared in 1939.1
Prototype
The prototype was designated the Ka-17, F1M1 by the military, and first flew in June 1936.1,2
Production
Production ended in March 1944.1
- Mitsubishi F1M1: 41,4
- Mitsubishi F1M2: 1,1141
- Mitsubishi: 5241
- Dai-Nijuichi: 5901
- Total: 1,1181,2
- Manufacturer: Mitsubishi Jukogyo K.K.2
Variants
- Mitsubishi Ka-17 / F1M1: Prototype.1,2 Had Nakajima Hikari 1 radial 9 engine (820 HP).1,2
- Mitsubishi F1M2: Increased vertical tail surfaces.1 Longer cowling.1 Straight taper wings.1 Wing dihedral was reduced.1,2
- Mitsubishi F1M2-K: Trainer.1,2 Converted from F1M2.1,2
Usage
Variety of Duties
The F1M was very versatile and was used as a coastal patrol, convoy escort, search and rescue, ocean patrol, transport, anti submarine, interceptor, dive bomber, and bombing.1 It could be operated from water bases and ships.1
The F1M was an aircraft carrier based aircraft that was used the most by the Imperial Japanese Navy.2 Eight battleships, nine cruisers, and six seaplane ships were equipped with the F1M2.2
Specifications
| Mitsubishi F1M1 | Mitsubishi F1M12 | Mitsubishi F1M21,2 | |
|---|---|---|---|
| Type | Reconnaissance floatplane1 | Reconnaissance2 | Reconnaissance2 |
| Crew | 21 | 22 | |
| Engine (Type) | Nakajima Hikari 12 | Mitsubishi Zuisei 131,2 | |
| Cylinders | Radial2 | Radial 141,2 | |
| Cooling | Air2 | ||
| Net HP | 8751,2 | ||
| Propeller blades | 2 metal2 | 31, 3 metal2 | |
| Dimensions | |||
| Span | 36' 2"2, 36' 11"1 11 m1 |
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| Length | 31' 2"1,2 9.5 m1 |
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| Height | 13' 1"2, 13' 1.5"1 4.02 m1 |
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| Wing area | |||
| Weight | |||
| Empty | 4,250 lb1 1,928 kg1 |
||
| Normal load | 5,622 lb1,2 2,550 kg1 |
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| Maximum load | 6,294 lb1 2,855 kg1 |
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| Performance | |||
| Speed @ 11,285' / 3,440 m |
230 mph1,2 370 kph1 |
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| Cruising speed | 127 mph1 204 kph1 |
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| Climb | 1,968'/minute1 600 m/minute1 |
||
| Climb to 9,840' / 3,000 m |
5.1 minutes1 | ||
| Climb to 16,405' / 5,000 m |
9.6 minutes1 | ||
| Service ceiling | 30,970'1,2 9,440 m1 |
||
| Range | 460 miles1,2 740 km1 |
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| Armament | 3: MG2 | ||
| Nose | 2: 7.7 mm MG1 | ||
| Rear cockpit | 1: 7.7 mm MG1 | ||
| Bombs | 132 lb2 | ||
| Bombs - under wings | 2: 132 lb1 2: 60 kg1 |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
- World War II Airplanes Volume 2, Enzo Angelucci, Paolo Matricardi, 1976
