World War II Bomber Aircraft

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 Japanese World War II Bomber Aircraft 


Kawasaki Ki-48 (Lily)
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The Kawasaki Ki-48 was a Japanese twin-engined light bomber that was used during World War II. Its Allied reporting name was "Lily."

The development of the aircraft began at the end of 1937 at the request of the Japanese military high command. Kawasaki received an order to develop a "high-speed bomber" capable of 480 km/h at 3,000 m (300 mph at 10,000 ft), and able to reach 5,000 m (16,400 ft) within 10 minutes. It was inspired by the Soviet Tupolev SB-2.

Kawasaki had the advantage of the experience of designing the Ki-45 twin-engined heavy fighter. Most technical problems were solved; however the aircraft had a number of defects. It could carry only a 800 kg (1,750 lb) bombload (less than the single-engined Typhoon fighter-bomber) and was equipped only with three machine guns, which made it very vulnerable to enemy fighters. The flight characteristics of the Ki-48 also left much to be desired. Allied fighters caught up in speed and eventually the KI-48 was too slow to outrun them. Despite the first versions being under-armoured, the KI-48 could loop and turn with an experienced pilot at the controls. Often the aircraft was used as a dive bomber in Burma. The aircraft was not necessarily a failure, and was considered an acceptable light bomber for the first few years of the war by many historians.

The aircraft served in China from late 1940, replacing the Kawasaki Ki-32, and were widely used in the Philippines, Malaya, Burma, New Guinea, the Solomon Islands and the Dutch East Indies, where the Ki-48 Ia and Ib models, slow and badly armed, were supplemented by the marginally improved Ki-48 IIa and IIc, which were maintained in service along the older types until the end of the war.

All models continued in service until the Battle of Okinawa during April 1945, when many were converted into Kamikaze aircraft (Ki-48-II KAI Tai-Atari) armed with an 800 kg (1,764 lb) bomb.

Ki-48 special attack unit

The British Pacific Fleet departed from Ceylon on 16 January 1945 en route to Australia, and struck Japanese-held oil wells and refineries at Palembang, Sumatra on 24-29 January 1945 in Operation Meridian.

On 29 January, seven Kawasaki Ki-48 of the Army's Shichisi Mitate Tokubetsu Kōgeki Tai counter-attacked the Allied fleet at low level as the British aircraft were returning from Palembang. The British radar picture was confused by the presence of over 100 friendly aircraft and the first two or three Supermarine Seafire CAP interceptions did not occur until just before the Ki-48 entered the air defence zone. The last pair of Seafires chased the five remaining Ki-48s inside the screen, and with the support of returning F4U Corsairs and F6F Hellcats which had just been scrambled, shot down all of them amongst intense AA fire. One Seafire was slightly damaged and one Hellcat was written off by friendly fire, but the only ship to be damaged was the carrier HMS IllustriousTemplate:WP Ships HMS instances, hit by heavy AA shells.

Such success, minor by Pacific fighting standards at the time, gave the British Pacific Fleet useful expertise and confidence in its ability to deal with kamikaze attacks.

General characteristics

  • Crew: Four
  • Length: 12.75 m (41 ft 9 in)
  • Wingspan: 17.45 m (57 ft 3 in)
  • Height: 3.8 m (12 ft 5 in)
  • Wing area: 40 m² (430.555 ft²)
  • Empty weight: 4,550 kg (10,031 lb)
  • Loaded weight: 6,500 kg (14,350 lb)
  • Max takeoff weight: 6,750 kg (14,881 lb)
  • Powerplant: 2× Nakajima Ha.115 [Nakajima_Ha-115_14cyl_radial]radial engines, 843 kW (1,130 hp) each

Performance

  • Maximum speed: 505 km/h (273 knots, 314 mph) at 5,600 m (18,375 ft)
  • Range: 2,400 km (1,296 nm, 1,491 mi)
  • Service ceiling 10,100 m (33,135 ft)

Armament
 

  • 3 × 7.7 mm (0.303 in) Type 89 [Type_89_Model_2_machine_gun]machine guns, in nose, dorsal and ventral positions
  • 800 kg (1,764 lb) of bombs

 


Mitsubishi G-3M (Nell)
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The Mitsubishi G3M (九六式陸上攻撃機: Type 96 land-based attack aircraft; Allied reporting name Nell) was a Japanese bomber aircraft used during World War II, mostly against the Chinese.

The bomber had a crew of five, and had its first flight in July 1935. The aircraft was armed with three 7.7mm machine guns. Maximum speed was 188 knots and had a range of over 2,200 miles. The G3M was also designed to carry an 800 kg torpedo for ship attacks.

The G3M has its origins in a specification submitted to the Mitsubishi company from the Imperial Japanese Navy requesting a heavy bomber aircraft with chiefly a range figure unprecedented at the time. This stemmed from principally Admiral Yamamoto's influence in the Naval High Commission of the necessity of a long range heavy bomber capable of encompassing the enormous ranges of the arenas where Imperial Japan sought to conquer in the years to come, including those outlined in the expansionist Tanaka Memorial -- namely China, Southeast Asia, the Pacific Isles and vast Far East Russia. The requirement for payload too, was unprecedented in Japanese military aviation history, though necessary to accommodate the aerial torpedo envisaged to combat the armoured battleships of the Allies in the geographical broadness of the Pacific front. The speed requirement submitted by the Naval Department was also unprecedented in not only Japanese but also international heavy bomber aviation, where in relation to the envisaged Japanese battlegrounds of China and the Pacific, the bomber would need to not only cover lengthy range, but necessarily feature the exceptional speed to strike distant targets with a minimum attack time. Thus the G3M was an embodiment of Japanese military aircraft design in the brief period leading to the Pacific War, with great offensive armament (in this case in the form of bombs/torpedoes), range and speed emphasised over protection and defensive capabilities.

The G3M flew for first time in 1935, taking off from a Nagasaki airfield belonging to Mitsubishi Heavy Industries and landing at Haneda Airport on the outskirts of Tokyo. The G3M first saw combat in Japan's expansionist campaigns on the Chinese mainland in what became known as the Second Sino-Japanese War, where as part of a pre-emptive strike plan designed by Admiral Yamamoto (the very authority that had demanded the designing of such a bomber), the G3M was able to exploit its long range capability,when August-November,1937 if established the "1st Rengo Kokutai" a special section conformed with "Kanoya" and "Kizarazu Kokutai" based in Taipei,Formosa, Omura,Kyūshū and Jeju Island.in August 14 of same year ones 42 "Nells" and 7 Hiro G2H1s scorted by 12 Nakajima A4Ns and 12 Mitsubishi A5Ms of "2nd Rengo Kokutai" (unit conformed by 12nd and 13th Kokutai),departing from bases for effectively crossing the East China Sea,for bombing Hangchow and Kwanteh,among others actions of terror bombing in coastal and inland targets in China, including the infamously treacherous bombing of the Battle of Shanghai and Nanjing. Thus while it was the first transoceanic bomber in air war history, it also had the dubious distinction of being the first mass-produced bomber aircraft to wage terror bombing indiscriminately on civilians. Later, from bases in occupied Chinese territories, it took part in the strategic carpet bombing of the Chinese heartland, its combat range being sufficient to cover the elongated distances involved. Most notably, it was involved in the round-the-clock Bombing of Chongqing, a campaign that resulted in what would now be considered massive collateral damage. When the Pacific War erupted in 1941 after a similarly Japanese-style pre-emptive strike in the Bombing of Pearl Harbor, although antiquated, 200 first line units were operated in the central Pacific and the Philippines. On the 8th of December 1941, (7th across the International Date Line), G3Ms struck Singapore City from bases in occupied Vietnam as one of many air raids during the Battle of Singapore, resulting in thousands of British and Asiatic civilians dead. Wake Island was similarly bombed by G3Ms on the first day of the war, with both civilian and US Navy infrastructure being heavily damaged on the ground.

The G3M was famous for taking part of the sinking of Prince of Wales and Repulse with the more advanced Mitsubishi G4M "Betty", on 10 December 1941. "Nells" provided important support during the attack on the HMS Prince of Wales and HMS Repulse (Force Z) near the Malayan coast. The Prince of Wales and the Repulse were the first two battleships ships ever sunk exclusively by air attack while at sea during war.

From 1943, the majority of "Nells" served as glider tugs, aircrew and paratroop trainers and for transporting high-ranking officers and VIPs between metropolitan islands, occupied territories and combat fronts until the end of the war.

General characteristics

  • Crew: 7
  • Length: 16.45 m (53 ft 11½ in)
  • Wingspan: 25 m (82 ft 0 in)
  • Height: 3.68 m (12 ft ⅞in)
  • Wing area: 75 m² (807 ft²)
  • Empty weight: 4,965 kg (10,923 lb)
  • Loaded weight: 8,000 kg (17,600 lb)
  • Powerplant: 2× Mitsubishi Kinsei 45 [Nakajima_Ha-115_14cyl_radial]radial engine, 1,075 hp (791 kW) each

Performance

  • Maximum speed: 375 km/h (203 knots, 233 mph)
  • Cruise speed: 280 km/h (151 knots, 174 mph)
  • Range: 4,400 km (2,730 mi)
  • Service ceiling 9,200 m (30,200 ft)
  • Rate of climb: 6 m/s (1180 ft/min)

Armament
 

  • Guns
    • 1 x Type 99 20mm [Type99mod2-20mm_Cannon]cannon in rear dorsal turret
    • 4 x Type 92 7.7 mm [Type92_7.7mm_Machine_Gun]machine gun in cockpit, left and right side positions, and in retractable forward dorsal turret.
  • Bombs
    • 800 kg of bombs or 1 torpedo

 


Mitsubishi G-4M (Betty)
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The Mitsubishi G4M or 一式陸攻 Ichishiki rikujō kōgeki ki, Isshikirikkō ("Type 1 land-based attack aircraft") was the main twin-engined, land-based bomber aircraft used by the Imperial Japanese Navy Air Service in World War II. The Allies gave the G4M the identification name of Betty.

The G4M had a long range and high-speed at the time of its introduction. However, it was known for its poorly-protected fuel tanks, which caused Allied fighter pilots to give it the derisive nicknames "one-shot lighter", "flying Zippo" and "flying cigar". Similarly, pilots of the Imperial Japanese Navy called the G4M the "Type One Lighter" and Hamaki (Cigar). This was due to the fact that on many occasions, it was used for low-altitude torpedo attacks where its performance advantages were negated. The "Betty"'s relatively-large size made it a large target to shoot at, and the simplified approach path on a torpedo run to attack a ship, meant for a generally easy interception.

When used for medium- to high-altitude bombing against stationary targets like a supply depots, seaports, or airfields, "ease of interception" was another matter entirely. Using its long range and high speed, the G4M could appear from any direction, and then be gone before many fighters could intercept them. The 20 mm cannon in the tail turret was much heavier armament than commonly installed in bombers, making dead astern attacks very dangerous. Sometimes, assuming they did not catch fire in the first place, G4Ms also proved to be able to remain airborne despite being badly shot up. For example, after 751 Kokutai's attack during the Battle of Rennell Island, three out of four survivors (of eleven aircraft that went to attack) returned flying on one engine only. Near the end of the war the "Betty" was used as a common kamikaze-carrying and launching platform, and was the usual aircraft for carrying the Ohka kamikaze rocket aircraft.

The G4M was similar in performance and missions to other contemporary twin-engine bombers such as the German Junkers Ju 88 and Heinkel He 111, the North American B-25 Mitchell, and the American Martin B-26 Marauder. These were all commonly used in the anti-shipping role, and all but the B-25 were used as torpedo-bombers. The G4M Model 11 was prominent in attacks on Allied shipping in the 1941 to early 1944 time-frame, but beyond that time, it was increasingly the easy prey of the ever-improving enemy fighters.

The G4M's baptism by fire occurred September 13, 1940 in Mainland China, when 27 Bettys and Mitsubishi C5M1 of 1st Rengo Kokutai (a composite force including elements of Kanoya and Kizarazu Kokutais) departed from Taipei, Omura and Cheju to attack Hankow. The bombers and reconnaissance aircraft were escorted by 13 Mitsubishi A6Ms of 12st Kokutai led by Navy Lt. Saburo Shindo. A similar operation occurred in May 1941. In December 1941, 120 Taiwan-based G4Ms of 1st Kokutai and Kanoya Kokutai belonging to the 21st Koku Sentai crossed the Luzon Strait en route to bombing the Philippines, the beginning to widespread Southeast Asia operations.

General characteristics

  • Crew: Seven (main-pilot, co-pilot, navigator/bombardier/nose gunner, captain/top turret gunner, radio operator/waist gunner, engine mechanic/waist gunner, tail gunner)
  • Length: 65 ft 6 in (19.970 m)
  • Wingspan: 81 ft 7 in (24.9 m)
  • Height: 16 ft 1 in (4.900 m (in a horizontal position))
  • Wing area: 840.9 ft² (78.125 m²)
  • Airfoil: Mitsubishi type
  • Empty weight: 15,430 lb (7,000 kg)
  • Loaded weight: 20,940 lb (9,5000 kg)
  • Powerplant: 2× Mitsubishi "Kasei (Fire star)" Type 11[Mitsubishi_Kasei_Type-11_14cyl_Radial], 14 cylinder radial engine, 1,530 hp () each
  • Propellers: Three-bladed Hamilton licensed Sumitomo constant speed variable-pitch

Performance

  • Maximum speed: 264.7 mph (426 km/h, 230 knots)
  • Cruise speed: 195.7 mph (315 km/h, 175 knots)
  • Stall speed: 74.6 mph (120 km/h)
  • Range: 2,664 mi, (overloaded, one way) (2,852 km, one way (overloaded: 4,288 km, 2,315 nm))
  • Service ceiling 27,890 ft (8,500 m)
  • power (detail):1,530 hp / 2,450 rpm at take-off, 1,410 hp / 2,350 rpm at 2,000 m, 1,340 hp / 2,350 rpm at 4,000 m (13,120 ft)

Armament

  • Guns: 1 x 20 mm Type 99 [Type99mod2-20mm_Cannon]cannon (tail turret), 4 x 7.7 mm Type 92 [Type92_7.7mm_Machine_Gun]machine gun (nose turret x 1, waist turret x 2, top turret x 1)

 

 

Mitsubishi Ki-21 (Sally)
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The Mitsubishi Ki-21 (九七式重爆撃機, Kyūnana-shiki jūbakugekiki?) (Allied codename: "Sally" /"Gwen") was a Japanese bomber during World War II. It began operations during the Second Sino-Japanese War participating in the Nomonhan Incident, and in the first stages of the Pacific War, including the Malayan, Burmese, Dutch East Indies and New Guinea Campaigns. It was also used to attack targets as far-flung as western China, India and northern Australia.

In 1936 Imperial Japanese Army Air Service issued a requirement for a new heavy bomber to replace both the Mitsubishi Ki-20 (Army Type 92 Heavy Bomber) and the Mitsubishi Ki-1 (Army Type 93 Heavy Bomber). The design called for a crew of at least four, top speed of 400 km/h (250 mph), endurance of at least five hours, and a bomb load of 750 kg (1650 lb). The design parameters were very ambitious, and few twin-engine bombers anywhere in the world could exceed such performance at that time.

Both Mitsubishi and Nakajima were asked to build prototypes. The Mitsubishi design was an all-metal cantilever mid-wing monoplane with retractable landing gear, ventral bomb bay and two radial engines. In the resulting competition Mitsubishi's Ki-21 and Nakajima's Ki-19 were found to have nearly identical performance. Although the Army liked the Ki-21 airframe, the Nakajima engines were considered superior, and after evaluation of both types, Mitsubishi was instructed to change its own 825 hp (620 kW) Mitsubishi Ha-6 radial engines for Nakajima Ha-5 engines and to modify its tail surfaces. The design was accepted into production as the "Army Type 97 Heavy Bomber Model 1A".

Production aircraft began to enter service in the summer 1938, replacing Fiat BR.20 bombers which had been purchased as an interim measure.

Several improved versions followed (see below) before the production of the type ended in September 1944. A total of 2,064 aircraft were built, 1,713 by Mitsubishi and 351 by Nakajima.

The Ki-21-Ia was used in combat in the war with China in autumn 1938, initially with great success, but not in great numbers, as production delays prevented the IJAAF from re-equipping the 60th Sentai and 61st Sentai until the end of 1939. However, combat revealed that the greatest weaknesses of the design were in its lack of armament and self-sealing fuel tanks.

The Ki-21-Ib was an improved version designed to address the armament issue by increasing the number of 7.7 mm Type 89 machine guns to five, and incorporating improvements to the horizontal tail surfaces and trailing edge flaps. In addition, the bomb bay was enlarged. The tail gun was a 'stinger' installation, and was remotely controlled. Also the fuel tanks were partially protected with laminated rubber sheets.

This was followed in production by the Ki-21-Ic with an auxiliary fuel tank of 110 Imperial gallons (500 liters), fitted in the rear weapons-bay and one more 7.7 mm machine gun, bringing the total to six. Four 50 kg (110 lb) bombs were carried externally. To offset the increase in weight the main wheels of the Ki-21-IC were increased in size.

However, by the attack on Pearl Harbor and the start of the Pacific War, losses due to improvements in Republic of China Air Force fighter quality and quantities caused losses to mount, and most Ki-21-1a, -1b and -1c had been relegated to training or second-line duties.

Front line units from mid-1940 were equipped with the Ki-21-IIa (“Army Type 97 Heavy Bomber Model 2A”) with the more powerful 1,500 hp (1,120 kW) Mitsubishi Ha-101 air-cooled engines and larger horizontal tail surfaces. This became the main version operated by most IJAAF heavy bomber squadrons at the beginning of the Pacific War, and played a major role in many early campaigns. For operations over the Philippines the JAAF's 5th,14rd and 62rd Air Groups, based in Taiwan, attacked American targets at Aparri, Tuguegarao, Vigan and other targets in Luzon on 8 December 1941. The 3rd, 12th, 60th and 98th Air Groups, based in French Indochina, struck British and Australian targets in Thailand and Malaya, bombing Alor Star, Sungai Petani and Butterworth under escort by Nakajima Ki-27 and Ki-43 fighters. However, starting from operations over Burma in December 1941 and early 1942, the Ki-21 began to suffer heavy casualties from Curtiss P-40's and Hawker Hurricanes.

To partially compensate, the IJAAF introduced the Ki-21-IIb, with a pedal-operated upper turret with one 12.7 mm (0.50 in) Type 1 machine gun, redesigned cockpit canopies and increased fuel capacity. Although used in all fronts in the Pacific theater, it became clear by 1942 that the design was rapidly becoming obsolete, and was increasingly shifted away from front-line service.

In spite of its shortcomings, the Ki-21 was remained in service until the end of the war, being utilized as transport (along with the civil transport version MC-21), bomber crew and paratrooper trainer, for liaison and communications, special commando and secret missions, and suicide operations.

Nine Ki-21-Ia/b were sold by Japan to Thailand in 1940 for use by the Royal Thai Air Force against Vichy French forces in French Indochina but did not participate in the French-Thai War as its crews had not completed training.

Towards the end of the war, remaining Ki-21s were used by Giretsu Special Forces in strikes against American forces in Okinawa and the Ryūkyū Islands. One of the noted operations was an attack on the Allied-held Yontan airfield on the night of 24 May 1945. Nine Ki-12-IIb's of 3rd Dokuritsu Chutai were dispatched for a strike, each with 14 commandos. Four were shot down, but five managed to crash-land on the airfield. The raiders, armed with submachine guns and phosphorous grenades then wrought havoc on the supplies and nearby aircraft, destroyed 70,000 gallons of fuel and nine aircraft, and damaging 26 more.

A number of Ki-21-la were modified to serve as military transports for use by Greater Japan Airways, which was under contract by the Japanese Army in China for transportation. Designated "MC-20", these aircraft had all armament and military equipment removed. Used primarily as cargo transports, each could also seat nine paratroopers. Aircraft built from the start as transports were given the separate designation of Mitsubishi Ki-57.

The Ki-21 had more than one Allied codename. Initially called 'Jane', the name was quickly changed to 'Sally' when General Douglas MacArthur objected that the name was the same as that of his wife. When the Ki-21-IIb entered service, the absence of the long dorsal “greenhouse” led Allied observers to mistake it for a completely new type, which was designated 'Gwen'. However, when it was realized that 'Gwen' was a new version of the Ki-21, it was renamed 'Sally 3', with 'Sally 1' referring to the earlier Ha-5 powered models, and 'Sally 2' referring to the Ha-101 powered Ki-21-IIa.

General characteristics

  • Crew: 5-7
  • Length: 16.0 m (52 ft 6 in)
  • Wingspan: 22.50 m (73 ft 10 in)
  • Height: 4.85 m (15 ft 11 in)
  • Wing area: 69.90 m² (752.12 ft²)
  • Empty weight: 6,070 kg (13,354 lb)
  • Loaded weight: 10,600 kg (23,320 lb)
  • plant: Power 2× Mitsubishi Type 100 Ha-101 [Mitsubishi_Ha-101_14cyl_Radial]14 cylinder radial, 1,119 kW (1,500 hp) each
  • Propellers: 2 three-blade metal variable-pitch propellers

Performance

  • Maximum speed: 485 km/h (301 mph) at 4,700 m (15,400 ft)
  • Cruise speed: 380 km/h (236 mph)
  • Range: 2,700 km (1,680 miles)
  • Service ceiling 10,000 m (32,800 ft)
  • Rate of climb: 13 min 13 sec to 6,000 m (19,680 ft)

Armament

  • 5 × 7.7 mm flexible Type 89 [Type_89_Model_2_machine_gun]machine guns in nose, tail, beam and tail positions
  • 1 × Ho 103 12.7 mm Type 1 [Ho-103_12.7mm_Machine_Gun]Heavy Machine Gun in dorsal turret
  • 1000 kg (2200 lb) of bombs


Mitsubishi Ki-30 (Ann)
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The Mitsubishi Ki-30 (九七式軽爆撃機, Kyunana-shiki keibakugekiki?) was a Japanese light bomber aircraft of World War II. It was a single-engine, mid-wing, cantilever monoplane of stressed-skin construction with a fixed tailwheel undercarriage and a long transparent cockpit canopy. The type had significance in being the first Japanese aircraft to be powered by a modern two-row radial engine. During the war, it was known by the Allies by the code-name Ann.

The Ki-30 was developed in response to a May 1936 Imperial Japanese Army specification to replace the Kawasaki Ki-3 light bomber with a completely indigenously designed and built aircraft. Mitsubishi and Kawasaki were requested to build two prototypes each by December 1936. The specification called for a top speed of 248.5 mph (400 km/h) at 9,845 feet; normal operating altitude from 6,560 feet to 13,125 feet, the ability to climb to 9,845 feet within 8 minutes and an engine to be selected from the 825 hp (620 kW)Mitsubishi Ha-6 radial, 850 hp (630 kW) Nakajima Ha-5 radial, or 850 hp (630 kW) Kawasaki Ha-9-IIb liquid-cooled inline engines, a normal bomb load of 661 lb (299.8 kg) and a maximum of 992 lb (450.0 kg), one forward-firing machine gun and one flexible rearward-firing machine gun, the ability to perform 60-degree dives for dive bombing, and a loaded weight less than 7,275 lb (3,299.9 kg).

The first Mitsubishi prototype flew on 28 February 1937 powered by a Mitsubishi Ha-6 radial. Originally, designed with a retractable main landing gear, wind tunnel tests indicated that the gain in speed was minimal due to the landing gear's extra weight and complexity and a fixed arrangement with “spatted” main wheels was chosen instead. The wing was mounted at a point above the line of the aircraft's belly in order fully enclose the bomb bay within the fuselage. The pilot sat just above the leading edge of the wing, and the rear-gunner/radio-operator just behind the wing trailing edge, in a long “greenhouse" canopy which gave both crewmen excellent all-around vision. The Ha-6 engine drove a three-bladed variable-pitch propeller.

Although this performed satisfactorily, a second prototype, fitted with a Nakajima Ha-5 engine was tested the same month.

Although behind schedule and overweight, both prototypes met or exceeded every other requirement. The second prototype's top speed of 263 mph (420 km/h) at 13,125 feet led the Imperial Japanese Army Air Force to place an order for 16 service trials machines. These were delivered in January 1938 and the result of the trials was that the Army ordered the Ki-30 into production in March under the designation Army Type 97 Light bomber.

Mitsubishi built 618 production machines through April 1940, and the First Army Air Arsenal at Tachikawa built 68 more by the time production ceased in September 1941. Including prototypes, a total of 704 Ki-30s were built.

The Ki-30s were first used in combat in Second Sino-Japanese War from spring 1938. It proved to be reliable in rough field operations, and highly effective while operating with fighter escort. This success continued in the early stages of the Pacific War, and the Ki-30s participated extensively in operations in the Philippines. However, once unescorted Ki-30s met Allied fighters, losses mounted rapidly and the type was soon withdrawn to second-line duties. By the end of 1942, most Ki-30s were relegated to a training role. Many aircraft were expended in kamikaze attacks towards the end of the war.

From late 1940, the Ki-30 was in service with the Royal Thai Air Force, and saw combat in January 1941 against the French in French Indochina in the French-Thai War. Additional Ki-30s were transferred from Japan in 1942.

General characteristics

  • Crew: 2, pilot and observer / bomb aimer
  • Length: 10.35 m (33 ft 11.5 in)
  • Wingspan: 14.55 m (47 ft 8.75 in)
  • Height: 3.65 m (11 ft 11.75 in)
  • Wing area: 30.58 m² (329.17 ft²)
  • Empty weight: 2,230 kg (4,916 lb)
  • Loaded weight: kg (lb)
  • Useful load: kg (kg)
  • Max takeoff weight: 3,320 kg (7,324 lb)
  • Powerplant: 1× Nakajima Ha-5-kai 14-cylinder radial, 708-kW (950-hp)

Performance

  • Never exceed speed: 442 km/h (knots, 275 mph)
  • Maximum speed: 423 km/h (knots, 263 mph)
  • Cruise speed: 380 km/h (knots, 236 mph)
  • Stall speed: km/h (knots, mph)
  • Range: 1,700 km (nm, 1,066 mi)
  • Service ceiling 8,570 m (28,115 ft)
  • Rate of climb: 8.33 m/s (1640 ft/min)
  • Wing loading: kg/m² (lb/ft²)
  • Power/mass: W/kg (hp/lb)

Armament

  • 2 × 7.7 mm (0.303-in) Type 89 [Type_89_Model_2_machine_gun]machine guns (one fixed wing-mounted and another manually aimed from the rear cockpit), 400-kg (882-lb) bombload.


Mitsubishi Ki-67 (Hiryu)

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The Mitsubishi Ki-67 Hiryū (飛龍, "Flying Dragon"; Allied code name "Peggy) was a twin-engined medium bomber produced by Mitsubishi and used by the Imperial Japanese Army Air Force in World War II. Its Army designation was "Type 4 Heavy Bomber" (四式重爆撃機).

The Ki-67 was the result of a 1941 Japanese army specification for a successor to the Nakajima Ki-49. This new aircraft was specified to be a high-speed heavy bomber with the maneuverability of a fighter. The Ki-67 was designed by Ozawa Kyonosuke, chief engineer at Mitsubishi, and was first encountered by Allied forces in a sea battle off Formosa in October 1944.

The Ki-67 had self-sealing fuel tanks and armor, features common in US fighters and bombers but frequently lacking in Japanese aircraft. With these features and its two 1,900 hp 18-cylinder air-cooled radial engines, the Ki-67 was perhaps one of the most sturdy and damage-resistant Japanese aircraft of WWII.

The Ki-67's bomb load of 1,070 kg (2,360 lb) (carried in its internal bomb bay) would classify it as a medium bomber for the US (the B-25 Mitchell could carry up to 6,000 lb, the B-26 Marauder up to 4,000 lb, and the A-20 Havoc up to 2,000 lb, for example). Its performance was remarkable compared to US medium bombers; the Ki-67 had a level-flight top speed of 334 mph (against 275 mph for the B-25, 287 for the B-26, and 338 for the A-20), good maneuverability in dives up to high speed (up to nearly 400 mph), excellent sustained rate of climb, and outstanding ability to turn (excellent turn rate, small turn radius, and ability to turn at low speeds). The maneuverability of the Ki-67 was so good that the Japanese used the design as the basis for the Ki-109 twin-engine fighter, originally designed as a night fighter, and later for use as a daylight heavy fighter. In the last stages of WWII, the Japanese Navy also used the design as the basis for the Q2M1 "Taiyo" radar-equipped anti-submarine plane.

Another interesting feature of the Ki-67 was that the gun in the dorsal gunner's turret position was a 20 mm cannon. (In addition to twin 12.5 mm machine guns in the tail, one 12.5 mm MG in the nose, and one 12.5 mm MG at each waist-gun position.) The 20 mm cannon is an unusually powerful defensive armament for a bomber. Until the introduction of the B-29 Superfortress, US bombers seldomly had cannon in defensive gunner positions, instead typically having one or two 0.50 caliber machine guns.

The Ki-67 was used for level bombing and (as the Yasakuni Type) torpedo bombing (it could carry one torpedo attached under the fuselage). The Ki-67 was initially used by the Japanese Army and Navy Air Services against the US Navy 3rd Fleet during its strikes against Formosa and the Ryukyu Islands. It was later used at Okinawa, in Mainland China,French Indochina,Karafuto and against B-29 airfields in Saipan, Tinian, and Guam in support of Giretsu (a special unit of the Japanese Imperial Army) strikes. One special ground-strike version used in the Giretsu missions was a Ki-67 I with three remote-control 20 mm cannons angled at 30 degrees for firing toward the ground, a 20 mm cannon in the tail, 13.2 mm machine guns in the lateral and upper positions, and more fuel capacity. Even with more fuel, the Giretsu missions were one-way only because of the long range. In the last stages of WWII, special attack versions of the Ki-67 (the I KAI and Sakura-dan models) were used in Kamikaze missions. (References include information from Lt. Sgt. Seiji Moriyama, a crew member in Fugaku Special Attack Unit, who witnessed Ki-67's being converted into To-Go suicide planes with two 800 kg bombs during Okinawa operations.)

By the end of WWII, 767 Ki-67's had been produced. Other sources relate that 698 Ki-67's were manufactured, excluding the KAI and Sakura-dan conversions.

General characteristics

  • Crew: 6-8
  • Length: 18.7 m (61 ft 4 in)
  • Wingspan: 22.50 m (73 ft 9 in)
  • Height: 7.70 m (25 ft 3 in)
  • Wing area: 66 m² (709 ft²)
  • Empty weight: 8,649 kg (19,068 lb)
  • Max takeoff weight: 13,765 kg (30,347 lb)
  • Powerplant: 2× Mitsubishi Ha-104 (army type 4) 18-cylinder radials, 1,417 kW (1,900 hp) each

Performance

  • Maximum speed: 537 km/h (334 mph)
  • Range: 3800 km (2,361 miles)
  • Service ceiling 9,470 m (31,070 ft)
  • Rate of climb: 450 m/min (1,476 ft/min)
  • Wing loading: 208 kg/m² (43 lb/ft²)
  • Power/mass: 0.21 kW/kg (0.13 hp/lb)

Armament

  • 1 × 20 mm Ho-5 [H0-5_20mm_Cannon]cannon in dorsal turret
  • 5 × 12.7 mm Type 1 [Ho-103_12.7mm_Machine_Gun]machine gun, one in nose, 2 in the tail, and 1 in each beam position
  • 1,070 kg (2,360 lb) of bombs in internal bay, some Kamikaze versions carried 6,000 lb (2,700 kg) of bombs

 


Nakajima Ki-49 (Donryu)
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The Nakajima Ki-49 Donryu (Name is from one of the virtuous buddhist priest Donryu: June 2 1556 - September 3 1623.) was a Japanese medium bomber of World War II. It was a twin-engine, mid-wing, cantilever monoplane of all-metal construction fitted with a retractable tailwheel undercarriage. During the Second World War, it was known to the Allies by the code-name "Helen".

The Ki-49 was designed to replace the Mitsubishi Ki-21, which entered service in the Imperial Japanese Army Air Force in 1938. Learning from service trials of the Ki-21, the Army realized that however advanced it may have been at the time, their new Mitsubishi bomber would in due course be unable to operate without fighter escorts. As a result the Japanese Army stipulated that its replacement should have the speed and defensive weaponry to enable it to operate independently.

The prototype first flew in August 1939 and the development programme continued through three prototypes and seven pre-production aircraft. This first prototype was powered by a pair of 708-kW (950-hp) Nakajima Ha-5 KA-I radial engines, but the next two had the 1,250 hp (932 kW) Nakajima Ha-41 engines that were inteded for the production version. Seven more prototypes were built, and these completed the test programme for the aircraft.

Eventually in March 1941, the Donryu went into production as the Army Type 100 Heavy Bomber Model 1.

Going operational from autumn 1941, the Ki-49 first saw service in China. After the outbreak of the Pacific War it was active in the New Guinea area and in raids on Australia. Like the prototype, these early versions were armed with five 7.7 (0.303 in) machine guns and one 20 mm cannon.

Combat experience in China and New Guinea showed the Donryu to be underpowered with bomb capacity and speed suffering as a result. Thus, in the spring of 1942 an up-engined version was produced, fitted with more powerful Ha-109 engines, and this became the production Army Type 100 Heavy Bomber Model 2 or Ki-49-IIa. The Model 2 also introduced improved armour and self-sealing fuel tanks and was followed by the Ki-49-IIb in which 12.7-mm (0.5-in) machine guns replaced three of the 7.7 mm (0.303-in) pieces.

In spite of these improvements however, losses continued to mount as the quantity and quality of fighter opposition rose. An attempt was made to stop the rot in early 1943 by further up-engining the type. This petered out, however, owing to development difficulties with the 2,420 hp (1,805 kW) Nakajima Ha-117 engines and the Ki-49-III never entered production with only six prototypes ever being built.

In the face of its increasing vulnerability to opposing fighter aircraft while performing its intended role, the Ki-49 was used in other roles towards the end of the Pacific War, including ASW patrol, troop transport and, ultimately, as kamikaze.

After 819 aircraft had been completed, production ended in December 1944.

General characteristics

  • Crew: 8
  • Length: 16.5 m (54 ft 1.5 in)
  • Wingspan: 20.42 m (67 ft 0 in)
  • Height: 4.25 m (13 ft 11.25 in)
  • Wing area: 69.05 m² (743.27 ft²)
  • Empty weight: 6,530 kg (14,396 lb)
  • Max takeoff weight: 11,400 kg (25,133 lb)
  • Powerplant: 2× Nakajima Ha-109 [Nakajima_Ha-109_14cyl_Radial]14-cylinder radial piston, 1,119-kW (1,500-hp) each

Performance

  • Maximum speed: 492 km/h (266 knots, 306 mph)
  • Cruise speed: 350 km/h (189 knots, 217 mph)
  • Range: 2,950 km (1,594 NM, 1,833 mi)
  • Service ceiling 9,300 m (30,510 ft)
  • Wing loading: kg/m² (lb/ft²)
  • Power/mass: W/kg (hp/lb)

Armament

  • Guns: 1 × 20 mm Type 99 [Type99mod2-20mm_Cannon]cannon, 5 × 7.7-mm (0.303-in) Type 89 machine guns.
  • Bombs: 1,000 kg (2,204-lb) bombload
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