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         The Nakajima Ki-49 was 
         designed as a replacement for the Mitsubishi Ki-21, which was just 
         entering service in the spring of 1938. The Japanese Army Air Staff 
         issued the specification at that very time, calling for a bomber 
         capable of operating without fighter escort, relying instead on heavy 
         defensive armament and high speed to escape interceptors. A maximum 
         speed of 311 miles per hour was requested, an improvement of about 16 % 
         over the Ki-21. Also included in the requirements were a range of 1,864 
         miles, a bomb load of 2,205 pounds, and a heavy (for the time) 
         defensive armament including one flexible 20mm cannon in the dorsal 
         position and several flexible 7.7mm machine guns, including a proper 
         tail turret (the first ever fitted to a JAAF bomber). Interestingly, 
         the specification called for crew armour and self-sealing fuel tanks-a 
         very welcome advance, considering the disdain the Japanese normally 
         showed for aircrew and fuel-tank protection. 
          
         When Nakajima lost the bomber competition in 1937 to Mitsubishi, they 
         had received a contract to build the Ki-21 in lieu of their own Ki-19, 
         and the Ki-49 design team, led by T. Koyama, used the opportunity to 
         study their competitor’s aircraft with a view toward improving on it 
         when they designed its intended replacement. Especial attention was 
         paid to handling, and a mid-mounted wing of low aspect ratio was 
         selected to ensure good manoeuvrability and stable flight at low and 
         medium altitudes.  
         The centre section of 
         the wing, inboard of the engine nacelles, was wider in chord than the 
         outer panels to accommodate six self-sealing fuel tanks, three on each 
         side of the fuselage. This also reduced drag and allowed the nacelles 
         to be positioned well ahead of the wing trailing edge. To improve 
         take-off and initial climb, Fowler flaps were adopted, and they 
         extended from the fuselage to the ailerons. In each of the outer wing 
         panels, two more self-sealing fuel tanks and a protected oil tank were 
         fitted. The defensive armament 
         was a single 20mm cannon mounted flexibly in the dorsal position and a 
         flexible 7.7mm machine gun in each of the nose, ventral, port and 
         starboard beam, and tail positions. The bomb bay was large, extending 
         almost the entire length of the wing centre section. All in all, the 
         new bomber looked very impressive when it was completed and flown for 
         the first time in August 1939.
          
         
           
         Natural-metal Ki-49s in formation over Japan.  
         Powered by two 950-hp 
         Nakajima Ha-5 radials, this first example was used primarily for 
         handling trials; service pilots were particularly impressed with the 
         prototype’s manoeuvrability, but complained that the Ki-49 was rather 
         underpowered when actually carrying a bombload, and was harder to fly 
         than the Ki-21. The second and third prototypes, powered by two 
         Nakajima Ha-41s of 1,250 horsepower, were completed and flown in the 
         final quarter of 1939. These were followed by seven pre-production 
         machines in 1940, and throughout that year and into the beginning of 
         1941, all ten Ki-49s were extensively tested. After minor modifications 
         in protection, armament, and seating arrangements, the type was 
         formally adopted by the Army in March 1941 as the Army Type 100 Heavy 
         Bomber Donryu (Storm Dragon) Model 1 (Ki-49-I). 
          
         While the service tests were proceeding with the first ten examples, 
         shocking reports were coming in from the Chinese battlefront. The Ki-21 
         was suffering heavy losses because the Army’s then-standard fighter, 
         the Nakajima Ki-27, lacked sufficient range to accompany the bombers 
         all the way to and from their targets. This created a delay in delivery 
         of the Ki-49 to front-line units, for valuable time was wasted in 
         trying to make a heavy escort-fighter version of the Donryu, the Ki-58.
          
         Three prototypes were 
         built between December 1940 and March 1941. The Ki-58 resembled the 
         Navy’s G6M in that it had the bomb bay sealed and replaced by a ventral 
         gondola; further armor protection was fitted, and the defensive 
         armament was increased to no less than five flexible 20mm cannon and 
         three 12.7mm machine guns. Fortunately, the idea was abandoned when 
         tests of the new Ki-43 Hayabusa proved it to have the range needed to 
         be a proper escort fighter. But further effort was diverted into the 
         building of a “formation leader’s” aircraft, the Ki-80; two prototypes 
         of this variant were built in October 1941, but further work on the 
         Ki-80 was cancelled by the coming of the war. The two prototypes 
         eventually were used as test-beds for the 2,420-hp Nakajima Ha-117 
         engine. 
          
         The Ki-49-I was first delivered to the JAAF in August 1941, and the 
         first unit to receive its Donryus was the 61st Sentai in China; because 
         of the low initial delivery rate, this group kept some of its older 
         Ki-21s until February 1942. In that same month, the Donryu made its 
         combat debut, in a raid on Darwin, Australia, on the 19th. Code-named 
         Helen, it was frequently encountered over New Guinea and New Britain. 
         But the doubts of the service-test pilots, alluded to above, were 
         confirmed by actual combat experience. In addition to its poor handling 
         and lack of power when fully loaded, the Ki-49’s speed, though superior 
         to the older type, was still not fast enough to avoid interception, and 
         its effective bomb load was lower than that of the Ki-21. On the plus 
         side, the Donryu’s crews thought highly of its superior defensive 
         armament and of its armour and self-sealing fuel tanks.  
         
           
         A Ki-49-I of the Hamamatsu Bomber School taking off.  
         In the spring of 1942, 
         it was decided to install a pair of 1,450-hp Nakajima Ha-109 radial 
         engines in the Ki-49 in an attempt to improve its performance and 
         handling. The oil coolers, formerly mounted on the front of the older 
         engines, were shifted to scoops under the cowlings; otherwise, there 
         was little change in the nacelles as the two kinds of engines were 
         virtually identical in size. Combat experience dictated further 
         changes, such as a new bombsight, heavier-grade armour plate, and 
         improved self-sealing fuel tanks. After testing of two pre-production 
         prototypes, the revised version was accepted for production as the 
         Ki-49-IIa, and deliveries commenced in September 1942. However, it was 
         swiftly realized that rifle-calibre machine guns were not very 
         effective against Allied fighters, and all of the former 7.7mm guns in 
         the nose, ventral, and tail positions were replaced by 12.7mm guns in 
         the major production variant, the Ki-49-IIb. 
          
         Despite all the improvements made to it, the Ki-49-II never totally 
         supplanted the Ki-21-II in service. It was the best-protected and 
         best-armed JAAF twin-engined bomber until the Mitsubishi Ki-67 Hiryu 
         was introduced in October 1944, but its crews were still disappointed 
         at its performance. In particular, its low and medium-altitude speeds 
         were still deemed unsatisfactory, and its flight characteristics were 
         not as pleasant as those of its predecessor. When the Americans 
         returned to the Philippines in October 1944, the Helen was very heavily 
         engaged; they suffered massive losses until December of that year when 
         most of the survivors were expended in suicide attacks against the US 
         landing force at Mindoro island. Many more were used in the suicide 
         attack role during the Okinawa campaign; for this mission all the 
         armament was removed, the crew was reduced to the two pilots only, and 
         the bomb load increased to 3,527 pounds.  
         
           
         A Ki-49-IIb abandoned in the Philippines, 1945.  
         Nakajima was baffled by 
         the type’s continuing problems, and tried hard to improve the Ki-49; 
         their most ambitious attempt involved creating a version featuring two 
         examples of the most powerful fourteen-cylinder radial engine ever 
         devised by any country, Nakajima’s own 2,420-hp Ha-117. But the 
         Ha-117’s teething troubles could never be resolved, and only six 
         examples of this subtype, the Ki-49-III, were built in 1943. 
          
         Despite its shortcomings, the Donryu was adapted to perform a number of 
         additional missions besides “heavy” bomber. Some were used as troop 
         transports (the great Navy ace Hiroyoshi Nishizawa was killed while 
         riding as a passenger in a Helen-ironic fate!); others were 
         field-modified as night fighters. In the night-fighter role, one 
         aircraft worked as a “hunter” with a searchlight, and a second was the 
         “killer”, mounting a 75mm cannon, but the Ki-49 made a disappointing 
         night fighter as it lacked the performance needed for this role. Still 
         others carried electronic and magnetic detection gear to act as 
         anti-submarine patrol planes. In the end, though, the Donryu was a very 
         disappointing aircraft, for all the effort put into making it an 
         effective warplane. Just 819 examples of the Ki-49 and its derivatives 
         were built, 769 by Nakajima, and 50 more by Tachikawa Aircraft Ltd., 
         but plans to also produce it in Harbin, Manchuria, by Mansyu were not 
         realized. Overall production ceased in December 1944, as the Army had 
         placed its hopes in the Mitsubishi Ki-67 Hiryu.  
         
           
         Close-up of a Ki-49-IIb warming up.  
         Nakajima Ki-49 Donryu 
         (Helen) Technical Data  
         Type:  
         Twin-engined “heavy” bomber, of all-metal construction. 
          
         Accommodation: 
         Crew of eight (two pilots, bombardier, navigator, radio 
         operator/gunner, and three dedicated gunners) all in enclosed cockpits, 
         main cabin, or turrets. 
          
         Powerplants:  
         (First prototype) Two Nakajima Ha-5 fourteen-cylinder air-cooled radial 
         engines, rated at 950 hp for take-off and 1,080 hp at 13,125 ft. 
          
         (Pre-production machines and Ki-49-I) Two Nakajima Ha-41 
         fourteen-cylinder air-cooled radials, rated at 1,250 hp for take-off 
         and 1,260 hp at 12,140 ft. 
          
         (Ki-49-II and Ki-58) Two Nakajima Ha-109 fourteen-cylinder air-cooled 
         radials, rated at 1,450 hp for take-off and 1,300 hp at 17,330 ft. 
          
         (Ki-48-III and Ki-80) Two Nakajima Ha-117 fourteen-cylinder air-cooled 
         radials, rated at 2,420 hp for take-off and 2,250 hp at 16,075 ft. 
          
         Armament: 
         (Prototypes/pre-production machines, Ki-49-I and Ki-49-IIa) One 
         flexible 20mm cannon in the dorsal position and one flexible 7.7mm 
         machine gun in each of the nose, ventral, beam, and tail positions. 
          
         (Ki-49-IIb and Ki-49-III) One flexible 20mm cannon in the dorsal 
         position, one flexible 12.7mm machine gun in each of the nose, ventral, 
         and tail positions, and one flexible 7.7mm machine gun in the port and 
         starboard beam positions. 
          
         (Ki-58) Five flexible 20mm cannon and three flexible 12.7mm machine 
         guns. 
          
         Bomb-load: 
         Normal, 1,653 lbs.; maximum, 2,205 lbs.; suicide attack, 3,527 lbs. 
          
         Dimensions, weights, and performance:  
          
         Ki-49-I: 
         Wingspan, 67 ft. 1/8 in.; 
         length, 55 ft. 1 ¾ in.; 
         height, 13 ft. 11 5/16 in.; 
         wing area, 743.245 sq. ft.; 
         empty weight, 13,382 lb.; 
         loaded weight, 22,377 lb.; 
         maximum weight, 23,534 lb.; 
         wing loading, 30.1 lb./sq. ft.; 
         power loading, 8.9 lb./hp; 
         performance figures N/A. 
          
         Ki-49-IIa: 
         Wingspan, 67 ft. 1/8 in.; 
         length, 54 ft. 1 5/8 in.; 
         height, 13 ft. 11 5/16 in.; 
         wing area, 743.245 sq. ft.; 
         empty weight, 14,396 lb.; 
         loaded weight, 23,545 lb.; 
         maximum weight, 25,133 lb.; 
         wing loading, 31.7 lb./sq. ft.; 
         power loading, 7.8 lb./hp; 
         maximum speed, 306 mph at 16,405 ft.; 
         cruising speed, 217 mph at 9,845 ft.; 
         climb to 16,405 ft., 13 min. 39 sec.; 
         service ceiling, 30,510 ft.; 
         normal range, 1,243 miles; 
         maximum range, 1,833 miles.  |