Japan's Mitsubishi Ki-21 bomber; Army Type 97
Allied code name: originally Jane, later Sally
Design
Designed to meet a Imperial Japanese Army Air Force requirement that was given in 19361 / 19382. It was to be a heavy bomber.2 It needed to operate at 6,500' - 13,000', fly 250 mph at 10,000', fly five hours at 187.5 mph, take eight minutes to climb 10,000', and take off in 975'.3
Competition
Both Nakajima and Mitsubishi submitted prototypes and they were tested for six months.3
The military ordered two more prototypes from each company and eventually decided on the Mitsubishi.3
Improvements
In 1939 Mitsubishi was instructed to improve the Ki-21 and they replaced the Ha-6 engine with a Ha-101 engine to give the Ki-21 more performance.1
Prototype
The first Ki-21 prototype first flew in November 19362 / on December 18, 19361,3.
Production
Produced by Mitsubishi and Nakajima.1 Production concluded in September 1944.2
- Mitsubishi Ki-21: 8:2
- Mitsubishi Ki-21-I: 7771
- Mitsubishi Ki-21-Ia, Mitsubishi Ki-21-Ib, Mitsubishi Ki-21-Ic: 7742
- Mitsubishi Ki-21-Ia:
- Production: November 1937 - ?3
- Mitsubishi Ki-21-Ib: 1203
- Mitsubishi Ki-21-Ic: 1603
- Mitsubishi Ki-21-II: 42, 1,2781
- First flew in December 1940.2
- Mitsubishi Ki-21-IIa: 5902,3
- Production: December 1940 - ?3
- Mitsubishi Ki-21-IIb: 6882,3
- Total: 2,0642,3
- Manufacturer: Mitsubishi2, Mitsubishi Jukogyo K.K.3, Nakajima2
- Production: March 1938 - September 19443
Variants
- Mitsubishi Ki-21: Prototype.2
- Mitsubishi Ki-21-I: Had Mitsubishi Ha-6 radial engines (850 HP).1 In mid 1938 deliveries started.2
- Mitsubishi Ki-21-Ia: Enlarged bomb bay.2
- Mitsubishi Ki-21-Ib: Better armament.3 Increased fuel.3
- Mitsubishi Ki-21-Ic: Larger wheels.2 Better armament.3 Increased fuel.2,3
- Mitsubishi Ki-21-II: Had Mitsubishi Ha-101 radial engines (1,500 HP).1 Horizontal tail surfaces were larger.2
- Mitsubishi Ki-21-IIa: Had a hand held 7.7 mm MG in rear dorsal position.1 Dorsal glasshouse replaced turret.2 Engines with more power.3 Landing gear modified.3
- Mitsubishi Ki-21-IIb: Had 12.7 mm MG in a turret in the dorsal position.1 Dorsal glasshouse replaced turret.2
- Mitsubishi MC-21: Transport.2 Converted from Ki-21-Ia in China.2
Usage
Arrival in China
The 60th and 61st Sentai went to China with their Ki-21s in 1938.1,2
Pacific War
The Ki-21 was the main bomber in December 1941.2 It was used in the Malayan, Thai, Burmese, and Netherlands East Indies campaigns.2,3
Secondary Roles
By 1943 the Ki-21 was obsolete and was moved into secondary rolls.2 These included being a bomber trainer, communication aircraft, and a suicide plane.2
Specifications
| Mitsubishi Ki-21 | Mitsubishi Type 97 | |
|---|---|---|
| Type | Medium bomber2 | Long range bomber4 |
| Crew | 5 - 72 | |
| Engine (Type) | 2: Mitsubishi Kinsei A-144 | |
| Cylinders | ||
| Cooling | ||
| Net HP | 870 each4 | |
| Propeller blades | ||
| Dimensions | ||
| Span | 73' 9.75"2 22.5 m2 |
85'4 |
| Length | 52' 6"2 16 m2 |
61'4 |
| Height | 15' 11"2 4.85 m2 |
|
| Wing area | ||
| Weight | ||
| Empty | ||
| Loaded | 24,000 lb4 | |
| Performance | ||
| Speed | 225 mph4 | |
| Climb | ||
| Service ceiling | ||
| Range | 2,500 miles4 | |
| Armament | 6: 7.7 mm MG2 | |
| Front | 2: MG4 | |
| Ventral | 2: MG4 | |
| Sides | 2: MG4 | |
| Tail | 1: MG4 | |
| Normal bomb load | 1,653 lb2 750 kg2 |
|
| Maximum bomb load | 2,205 lb2 1,000 kg2 |
4,400 lb4 |
| Mitsubishi Ki-21-I | Mitsubishi Ki-21-Ia | |
|---|---|---|
| Type | ||
| Crew | ||
| Engine (Type) | 2: Nakajima Ha-5 Kai2 | |
| Cylinders | Radial 142 | |
| Cooling | ||
| Net HP | 1,080 each2 | |
| Propeller blades | 3 each2 | |
| Dimensions | ||
| Span | ||
| Length | ||
| Height | ||
| Wing area | ||
| Weight | ||
| Empty | 10,342 lb2 4,691 kg2 |
|
| Loaded | 17,452 lb2 7,916 kg2 |
|
| Performance | ||
| Speed @ 13,125' / 4,000 m |
268 mph2 431 kph2 |
|
| Climb | 1,150'/minute2 350 m/minute2 |
|
| Service ceiling | 28,215'2 8,600 m2 |
|
| Range | 932 - 1,678 miles2 1,500 - 2,700 km2 |
|
| Armament |
| Mitsubishi Ki-21-II | Mitsubishi Ki-21-IIb | |
|---|---|---|
| Type | Bomber1,3 | |
| Crew | 51,3 | |
| Engine (Type) | 2: Mitsubishi Ha-1012 | 2: Mitsubishi Ha-101 piston1,3 |
| Cylinders | Radial 142 | Radial 143 |
| Cooling | Air3 | |
| Net HP | 1,500 each2 | 1,500 each1,3 |
| Propeller blades | 3 each2 | |
| Dimensions | ||
| Span | 73' 9"3, 73' 9.75"1 22.5 m1 |
|
| Length | 52' 5 7/8"1, 52' 6"3 16 m1 |
|
| Height | 15' 10 7/8"1, 15' 11"3 4.85 m1 |
|
| Wing area | 749.2 ft2 1 69.6 m2 1 |
|
| Weight | ||
| Empty | 13,382 lb1,2 6,070 kg1,2 |
|
| Loaded | 21,362 lb3, 23,391 lb1,2 10,610 kg1,2 |
|
| Performance | ||
| Speed @ 13,125' / 4,000 m |
302 mph1 486 kph1 |
|
| Speed @ 14,485' / 4,720 m |
302 mph2 486 kph2 |
|
| Speed @ 15,485' | 302 mph3 | |
| Climb | 1,640'/minute2 500 m/minute2 |
|
| Climb to 19,685' / 6,000 m |
13.2 minutes1 | |
| Service ceiling | 32,810'2 10,000 m2 |
32,810'1,3 10,000 m1 |
| Range | 1,680 miles2 2,700 km2 |
1,680 miles1,3 2,700 km1 |
| Armament | 6: MG3 | |
| Bombs | 2,200 lb3 |
Sources:
- Fighting Aircraft of World War II, Editor: Karen Leverington, 1995
- Aircraft of WWII, Stewart Wilson, 1998
- World War II Airplanes Volume 2, Enzo Angelucci, Paolo Matricardi, 1976
- Aeronautics Aircraft Spotters' Handbook, Ensign L. C. Guthman, 1943
