The Kawasaki Ki-48 was a nicely 
          designed aircraft, fast, manoeuvrable, and well armed both offensively 
          and defensively-for its time, which was the late 1930s and up 
          through early 1942. Then, the changing pattern of the air war over the 
          Pacific-Asian battlefronts, and the changing operational requirements, 
          left this trim little twin-engined light bomber behind. Although its 
          production ended in October 1944 with 1,977 examples built, it 
          remained in service because, by that date, Japan was plainly losing 
          the war, and was in dire need of virtually anything that could 
          fly-particularly for "special" (suicide) attacks.
          Early in the Sino-Japanese War of 
          1937, China deployed numbers of Russian-built Tupolev SB-2 light 
          bombers, sometimes crewed by Soviets, on hit-and-run attacks against 
          the Japanese invaders. The Japanese were surprised by this aircraft's 
          speed; it was faster than the Ki-10 biplane fighter, and was nearly as 
          fast as the Ki-27 monoplane fighter which was just entering service 
          with the Japanese Army Air Force. Certain air staff officers were so 
          impressed by the SB-2's performance that they obtained the go-ahead to 
          begin development of a similar light bomber for the JAAF. Kawasaki 
          Aircraft Ltd. was issued the specifications in December 1937. These 
          called for a twin-engined light bomber with (a) a top speed of 298 mph 
          at 9,845 feet; (b) a cruising speed at the same altitude of 217 mph; 
          (c) climb to 16,405 feet in 10 minutes; (d) a bombload of 882 pounds; 
          (e) engines to be Nakajima Ha-25 radials; (f) defensive armament of 
          three or four flexible 7.7mm machine guns; and (g) ability to operate 
          under the extreme winter conditions prevailing in Manchuria and North 
          China. 
          Actual design work began in January 
          1938 with Dr. Takeo Doi in charge, but because he was also in charge 
          of the Ki-45 twin-engined fighter design team, and the Ki-45 had a 
          higher priority, the first prototype of the new light bomber wasn't 
          ready for flight until more than a year and a half passed, in July 
          1939. Experience gained from designing the Ki-45 was incorporated into 
          the bomber project. The cantilever wing was mid-mounted to allow an 
          internal bomb bay. The crew of four was to consist of the pilot, a 
          bombardier/nose gunner with a 7.7mm weapon at his disposal, a 
          radio-operator/gunner manning the dorsal 7.7mm machine gun, and a 
          navigator/gunner utilizing the ventral 7.7mm gun. Normal bombload was 
          to be twenty-four 33-lb. bombs or six 110-lb. bombs, and the twin 
          engines were, as per the requirements, Nakajima Ha-25s driving 
          three-bladed variable-pitch propellers. 
          
          
          Ki-48 parked at a forward airfield in either China or the Philippines, 
          1944.
          During the prototype's flight trials, 
          it easily met all performance requirements and won praise from Army 
          test pilots for its manoeuvrability and handling characteristics, but 
          it suffered from severe tail flutter. Five further prototypes, built 
          between September and November of 1939, tested various tail-surface 
          modifications, until it was found that raising the horizontal 
          stabilizers approximately 13 ¾ inches and generally strengthening the 
          rear fuselage was the combined solution to the flutter problem. Very 
          late in 1939, quantity production of the new light bomber commenced 
          under the designation Army Type 99 Twin-Engined Light Bomber Model 
          1A, or Ki-48-Ia. 
          
          The first production Ki-48-Ia was 
          completed in July of the next year, and by that autumn, the 45th 
          Sentai (Group) was re-equipped with the new aircraft and deployed 
          to the North China battlefront, where the Ki-48 swiftly won a high 
          reputation with its crews. Facing largely token Chinese opposition, 
          the Ki-48 performed satisfactorily, winning much praise for its high 
          speed. In addition to daylight tactical sorties, night strategic 
          attacks were pioneered by the 45th Sentai, in preparation for 
          similar attacks on the forces of the Western Allies in the upcoming 
          Pacific War. Late production Ki-48-Is were designated Ki-48-Ib, 
          differing from the earlier model solely in having minor internal 
          equipment changes and improved machine gun mountings. 
          When the Pacific War began, the Ki-48 
          was the most important JAAF light bomber outside the Chinese front; 
          the older single-engined Ki-30 and Ki-32 were retained for China 
          service. Aircraft of the 8th, 27th, 75th, and 90th Sentais were 
          deployed against Commonwealth forces in Malaya and Burma, and against 
          the Americans in the Philippines, before being transferred to the 
          Dutch East Indies, and later to New Guinea. But against Allied 
          fighters of more modern vintage, the Ki-48-I fared badly; the high 
          turn of speed it was so praised for over China was too low to allow 
          the Lily, as the Allies code-named it, to avoid interceptors. Also, 
          its defensive armament was wholly inadequate, its bomb load was too 
          small, and it lacked any form of crew or fuel-tank protection. To 
          limit combat losses, the early model Lilies were used for night 
          attacks whenever possible, reducing their effectiveness even more.
          
          
          
          Close-up of the Ki-48's ventral gun position.
          An improved model of the Lily 
          was already being developed as the Pacific War commenced. The 
          Ki-48-II differed little from its predecessor, but it incorporated 
          a slightly lengthened fuselage, improved engines (Nakajima Ha-115s 
          with a two-stage blower), some fuel-tank protection, and some armour 
          for the crew, including a 12.5mm plate behind the bombardier's seat, a 
          6.5mm plate under the pilot's seat, 16.5mm armour behind the pilot's 
          seat, and 16.5mm plates to protect the dorsal and ventral ammunition 
          boxes. Within two months of its first flight, the Ki-48-II entered 
          production as the Ki-48-IIa. These production planes differed 
          from the prototypes only in minor details, such as local strengthening 
          of the fuselage. The Ki-48-IIb was a dive bomber, fitted with 
          retractable dive brakes under the outer wings (these were of the 
          "snow-fence" variety). 
          The maximum bomb-load of the Ki-48-II 
          was double that of the -I, but it was still a great deal less than 
          that of the standard Allied light bomber, the A-20 Havoc. And although 
          the speed of the Ki-48-II was superior to that of the -I, it was still 
          not fast enough to outrun the improved Allied fighters of the 
          later-war period. But its worst failing was its woefully inadequate 
          defensive armament, which had not been improved since the prototype 
          first flew. The Lily proved to be "easy meat" in the air, and 
          large numbers were also destroyed on the ground in New Guinea despite 
          Japanese efforts to disperse and camouflage the planes on their jungle 
          airstrips.  
          An attempt to fit a single example of 
          the Lily with a 20mm cannon in a revolving turret was 
          unsuccessful due to the increased weight and the complication of such 
          a fitting on a plane as small as the Ki-48. The final production 
          variant, the Ki-48-IIc, received a 12.7mm machine gun in a 
          flexible dorsal mounting, plus a second nose-mounted 7.7mm machine 
          gun; the bombardier could use either gun as needed. Still, despite all 
          attempts to keep the Ki-48 a viable warplane, it was obvious the type 
          was obsolescent, and so production ended in the autumn of 1944, as 
          noted above. Some Ki-48-IIs continued to serve in a conventional 
          bombing role, mainly at night, in the Philippine and Okinawan 
          campaigns. But most surviving Lilies were expended in daylight 
          suicide attacks in the latter campaign, usually en masse, in 
          the Kikusui (Floating Chrysanthemum) raids. A number of 
          Ki-48-IIs were modified as Ki-48-II-KAI special attack planes 
          by the Army Air Arsenal at Tachikawa. These carried a 1,764-lb. 
          bombload, triggered upon contact with the target by means of a long 
          rod protruding from the aircraft's nose like a mosquito's proboscis.
          
          
          
          Ki-48 abandoned in the Philippines, 1945.
          Four Ki-48-IIbs were used in 1944 to 
          test the Kawasaki I-Go-I-B air-to-surface guided missile, and another 
          Ki-48-II was used to test the experimental Ne-O turbojet in flight; to 
          accomplish this, the bomb-bay doors were removed and the jet engine 
          was slung under the fuselage. In addition, two proposed but 
          never-built variants were the Ki-81 formation commander's aircraft, 
          heavily armed and armoured; and a single-seat special attack aircraft, 
          the Ki-174.  
          
           Kawasaki Ki-48 (Lily) Technical Data
           Type: 
           
           Twin-engined light bomber, of all-metal construction with 
           fabric-covered control surfaces. 
           
           Accommodation: 
           Crew of four in enclosed cockpit/cabin. 
           
           Powerplant: 
           (Prototypes and Ki-48-I) Two Nakajima Ha-25 fourteen-cylinder 
           air-cooled radial engines, rated at 1,000 hp for take-off and 980 hp 
           at 9,845 ft. 
           
           (Ki-48-II) Two Nakajima Ha-115 fourteen-cylinder air-cooled radials, 
           rated at 1,130 hp for take-off, 1,070 hp at 9,185 ft., and 950 hp at 
           18,375 ft. 
           
           Armament: 
           (All except Ki-48-IIc) Three flexible 7.7mm machine guns, one each in 
           the nose, dorsal, and ventral positions. 
           
           (Ki-48-IIc) Two nose-mounted flexible 7.7mm machine guns, one 
           ventral-mounted flexible 7.7mm machine gun, and one dorsal-mounted 
           flexible 12.7mm machine gun. 
           
           Bomb load: 
           (Ki-48-I) Normal, 661 lb.; maximum, 882 lb. (Ki-48-II) Normal, 882 
           lb.; maximum, 1,764 lb. 
           
           Dimensions, weights, and performance: 
           
           Ki-48-I: 
           Wingspan, 57 ft. 3 25/32 in.; 
           length, 41 ft. 1 1/16 in.; 
           height, 12 ft. 5 19/32 in.; 
           wing area, 430.555 sq. ft.; 
           empty weight, 8,929 lb.; 
           loaded weight, 13,007 lb.; 
           maximum weight, 13,338 lb.; 
           wing loading, 30.2 lb./sq. ft.; 
           power loading, 6.5 lb./hp; 
           maximum speed, 298 mph at 11,485 ft.; 
           cruising speed, 217 mph at 11,485 ft.; 
           climb to 16,405 ft., 9 minutes; 
           service ceiling, 31,170 ft.; 
           normal range, 1,230 miles; 
           maximum range, 1,491 miles. 
           
           Ki-48-II: 
           Wingspan, 57 ft. 3 in.; 
           length, 41 ft. 9 31/32 in.; 
           height, 12 ft. 5 19/32 in.; 
           wing area, 430.555 sq. ft.; 
           empty weight, 10,031 lb.; 
           loaded weight, 14,330 lb.; 
           maximum weight, 14,881 lb.; 
           wing loading, 33.3 lb./sq. ft.; 
           power loading, 6.3 lb./hp; 
           maximum speed, 314 mph at 18,375 ft.; 
           cruising speed N/A; 
           climb to 16,405 ft., 8 min. 30 sec.; 
           service ceiling, 33,135 ft.; 
           normal range, 1,274 miles; 
           maximum range, 1,491 miles.