Friday, August 14, 2015

Kayaba Ka-1




The Imperial Japanese Army became interested during the late 1935 in autogyro developments taking place in the USA and, believing that such an aircraft might be developed for use as an artillery spotter, imported from America in 1939 a Kellett KD-1A. However, soon after this aircraft had arrived in Japan it was irreparably damaged during a flight test and the army arranged for the wreck to be transferred to the Kayaba Industrial Company, which had been carrying out research into the autogyro configuration. Shortly afterwards Kayaba was requested to proceed with design and development of a two-seat autogyro based on the Kellett. The resulting Kayaba Ka-1 prototype comprised a fuselage with two separate open cockpits in tandem, a tail unit incorporating a tailplane with twin inverted fins, fixed tailwheel landing gear, and an Argus As 10c engine mounted conventionally in the nose of the fuselage to drive a two-blade tractor propeller; the pylon for the three-blade unpowered rotor was incorporated in the fuselage structure, mounted just forward of the front cockpit.

First flown on 26 May 1941, the Ka-1 proved successful in early flight testing, and the type was ordered into production to serve in the originally intended role as a spotter-plane for artillery units. At the same time Japanese shipping losses were beginning to rise and it was suggested that the very short takeoff required by such aircraft would make them suitable for operation from the light escort carrier Akitsu Maru. A few production Ka-1s were modified for this role and equipped to carry two 132-lb (60-kg) depth charges, but because of their limited payload capability these had to be flown as single-seaters. Operating for some time off Japanese coastal waters they were the world's first operational armed rotary-wing aircraft, with production of both versions totalling approximately 240. This number included one Ka-1 KAI which was tested with rockets attached to the rotor tips in an attempt to improve payload capability, and a single aircraft that was evaluated with a 240-hp (179-kW) Jacobs L-4MA-7 7-cylinder radial engine, allocated the designation Ka-2.

Technical data for  Kayaba Ka-1
General characteristics
    Crew: 1-2
    Length: 9.2 m (30 ft 2⅛ in)
    Rotor diameter: 12.2 m (40 ft 0¼in)
    Disc area: 117 m² (10.9 ft²)
    Empty weight: 775 kg (1,709 lb)
    Max takeoff weight: 1,170 kg (2,574 lb)
    Powerplant: 1× Argus As 10c air-cooled inverted V8 engine, 180 kW (241 hp)
Performance
    Maximum speed: 165 km/h (89 knots, 102 mph)
    Cruise speed: 115 km/h (62 knots,71 mph)
    Range: 280 km (151 nm, 174 mi)
    Service ceiling: 3,500 m (11,500 ft)
    Rate of climb: 5 m/s (980 ft/min)
Armament
    1x 60 kg (132 lb) depth charges

Nakajima Kikka* [Kitsuka]




The Kikka (Orange Blossom), though a bit smaller than the Messerschmitt Me 262, was clearly inspired by the German jet fighter. Its primary claim to fame is that it was the very first Japanese aircraft to take off under jet power, even if it did so only once. Aside from that, it was yet again a case of too little, too late, since only the one prototype actually flew, although a second one was just a few days short of readiness when Japan capitulated.

Enthusiastic reports from the Japanese air attaché in Berlin on the development of the Me 262 led the Naval Air Staff, in September of 1944, to instruct Nakajima to design and build a similar aircraft for use as a high-speed attack bomber relying on speed to evade interceptors. The formal requirements included the following: (a) a top speed of 432 mph; (b) a range of 127 statute miles with a 1,102-lb. bombload, or 173 st. miles with a 551-lb. bombload; (c) a landing speed of 92 mph; and (d) a take-off run of just 1,150 feet when using two 992-lb. thrust RATOG bottles under the wings. Additionally, the new jet was to be easily built by semi-skilled labour, and the outer wing panels were to be foldable, enabling the aircraft to be concealed in caves and tunnels.

Designers Kazuo Ohno and Kenichi Matsumura created a plane that could be called a 2/3 rd or ¾ th-scale mimic of the Messerschmitt fighter. Whereas the Me 262 had a wingspan of about 40 feet and a length of around 34 feet, the Japanese aircraft was just a bit over 26 ½ feet long with a wingspan of just over 32 ¾ feet. Its wing was nicely swept, but the tail surfaces were not, and all control surfaces were, oddly enough, fabric-covered in an otherwise-all-metal airplane. The canopy was a three-piece sliding type, instead of the Messerschmitt’s three-piece hinged “coffin-lid” arrangement.

The twin turbojets were mounted beneath the wings in separate nacelles, allowing, with a minimum of changes, the installation of a variety of engines as they were developed. As it turned out, this feature was quite useful, as engine development fell behind that of the airframe. Initially, the plane was to have been powered by two Campini-type Tsu-11 engines, but these were replaced by a pair of 750-lb. thrust Ne-12 turbojets. But the future of the Navy Special Attacker Kikka (as it was designated) was made uncertain by the failure of the Ne-12 to develop its designed power during ground tests. By a stroke of luck, Engineer Eichi Iwaya of the Navy had obtained detailed photographs of the BMW 003 axial-flow turbojets used in the Me 262, and from those photos the Japanese were able to create a similar engine, designated Ne-20, with a theoretical power output of 1,047 pounds of static thrust. Everyone concerned felt the Ne-20 was perfect for the Kikka, and so the project’s pace was speeded up during the summer of 1945.

At this point, a note about the aircraft’s designation would be in order. Although it was dubbed a "Special Attacker", this writer believes that the Kikka was not actually intended for kamikaze attacks, except in extremis (i.e., if the pilot were wounded or the airplane was damaged, and could not return to base). It seems very foolish to go to the trouble to design a very expensive jet-powered plane and then assign it to one-way missions. The Me 262 was notorious for requiring a skilled pilot to fly it, and even then the pilot, if he had previous experience in aircraft with reciprocating engines, had to unlearn a lot of habits which were all right for flying conventional fighters but which could be fatal in the 262. For example, the Me 262’s throttles could not be “chopped”, i.e., quickly brought from high power to a lower-power setting, or shoved forward swiftly, “balls to the wall” as American flying slang put it.
Jet throttles had to manipulated carefully and slowly, or else the jet engines would flame out, either from fuel starvation or fuel satiation. Thus, by analogy, only skillful pilots could fly the Kikka. 

Undoubtedly the Japanese were aware, from reports from their air attaché in Germany, of the unique problems involved in flying a jet as opposed to flying a more conventional aircraft. Thus, the Kikka could not have been intended as a kamikaze aircraft. Indeed, it was intended for other roles besides being a fast attack bomber, as will be seen. The term “Special Attacker” refers, in this writer’s opinion, to the special way the Kikka was powered (by jets) rather than to its being intended for “special”, i.e., suicide, attacks.

With its Ne-20 engines installed, the Kikka prototype was given its first ground tests on June 30, 1945. Late in July, it was dismantled and taken to Kisarazu Naval Airfield, where after re-assembly it was flown for the first time on August 7, with Lt. Cdr. Susumu Takaoka as test pilot. The Kikka taxied for a long time before it gained enough speed to lift off the ground; the flight itself lasted just 20 minutes, and the aircraft was never taken above 2000 feet. The slowness with which it gained take-off speed delayed the second flight until August 11, when it attempted to lift off with RATOG bottles beneath the wings. Unfortunately, the rocket bottles were not installed at the correct angle to lift the Kikka off the runway, and after the rockets burned out, the pilot aborted the take-off and crashed into the rough ground beyond the runway’s end. The second prototype was almost ready for its own first flight when the war ended on August 15. Eighteen additional prototypes and pre-production examples were left in various stages of construction on that date.

Aside from the basic attack bomber, there was a projected unarmed two-seat trainer, and the third Kikka was to be the prototype for this variant. An unarmed two-seat reconnaissance version and a cannon-armed single-seat fighter were also under development at the war’s end. The fighter variant was to have been powered by either a pair of 1,984-lb. thrust Ne-130 or a pair of 1,951-lb. thrust Ne-330 axial-flow turbojets, and armed with a pair of nose-mounted 30mm cannon.

Nakajima Kikka Technical Data
Type:
Single-seat twin-jet attack bomber, of all-metal construction with fabric-covered tail surfaces.
Accommodation:
Pilot in enclosed cockpit.
Powerplant:
Two Ne-20 axial-flow turbojets, rated at 1,047-lb. of static thrust.
Armament: One 1,102-lb. or 1,764-lb. bomb under the fuselage centre section.
Dimensions, weights, and performance:
Wingspan: 32 ft. 9 11/16 in.;
length, 26 ft. 7 7/8 in.;
height, 9 ft. 8 5/32 in.;
wing area, 142.083 sq. ft.;
empty weight, 5,071 lb.;
loaded weight, 7,716 lb.;
maximum weight, 8,995 lb.;
wing loading, 54.3 lb./sq. ft.;
power loading, 3.7 lb./lb. s. t.;
maximum speed, 387 mph at sea level, (estimated) 433 mph at 32,810 ft.;
(estimated) climb to 32,810 ft., 26 minutes;
(estimated) service ceiling, 39,370 ft.;
(estimated) range, 586 statute miles.


In the section devoted to this aircraft he refers to the aircraft as the Nakajima Kitsuka (I had always thought it the Kikka).

At the end of the section he says this .....

'A note about the use of the name Kitsuka as opposed to the more commonly used Kikka. Kitsuka is the proper translation of the kanji characters. However, it is pronounced 'kikka'. Kikka was used in post-war reports as phonetically it approximated to Kitsuka and thus has become the accepted name of the aircraft. Neither name is incorrect.'

Now, quite apart from the fact that our high school teachers would be aghast at the last sentence containing a double negative, I would have thought that the translation of kanji characters in an English language book would be phonetic (the same as Russian words and names are) with perhaps slight differences in spelling.

So how then do you get Kitsuka pronounced Kikka if it isn't Kikka......As I see it Kitsuka has 3 syllables and Kikka has 2? 

If Kitsuka is pronounced Kikka, then if someone asks me what this aircraft is then should I say Nakajima Kikka, but write down Nakajima Kitsuka?

Friday, July 24, 2015

China Expedition



While they had been manufacturing Western designs under license in the 1920s, Japanese aircraft builders had been catching up on the fine points of aeronautical design. In the early 1930s, they were ready to proceed with designs of their own.

In February 1934, Imperial Navy air headquarters issued a 9-shi specification calling for a new single-seat fighter. Although carrier-based capability was virtually implicit in a navy requirement, one of its chief architects, Lt. Cmdr. Hideo Sawai, had deliberately avoided specific reference to such characteristics, concerned that it would inhibit the designers. In contrast to British and American naval aviation planners, Sawai wanted the manufacturers to produce a high-performance fighter that would bring Japan up to world standard—the matter of adapting and equipping it for operations from carrier decks would be dealt with afterward. The specification called for a maximum speed of 350 kilometers per hour (217 miles per hour) at 3,000 meters (9,840 feet) and the ability to climb to 5,000 meters (16,405 feet) within 6.5 minutes. Armament was to consist of two 7.7mm machine guns, wingspan would not exceed 11 meters (36 feet), and length no more than 8 meters (26 1/2 feet).

Among those who sought to meet the requirement was Mitsubishi’s chief designer, Jiro Horikoshi. After giving cursory consideration to other configurations, Horikoshi determined that the fighter must be a low-wing monoplane, with attention paid to the cleanest possible aerodynamics and to the minimum possible weight. The airframe he designed used stressed-skin aluminum over a two-spar box-type wing structure of inverted gull form, which was later altered into a flat center section with dihedral for the outer wing panels. After considering the possibility of incorporating retractable landing gear into his design, Horikoshi rejected it on the grounds that the 10 percent decrease in drag would result in only a 3 percent increase in speed, not enough to justify the system’s greater weight and complexity. Instead, his monoplane would have fixed undercarriage, with streamlined fairings over the wheels.

The first Ka-14 prototype, powered by a 550-horsepower Nakajima Kotobuki 5 nine-cylinder radial engine, was completed in January 1935, just eleven months after Mitsubishi received the 9-shi specification. During its first flight tests in February, it reached a speed of 444 kilometers per hour (276 miles per hour) at 10,500 feet, exceeding both the navy’s requirement and Horikoshi’s own expectations. Nevertheless, the Ka-14 had a great obstacle to overcome when it competed with the Nakajima A4N1 biplane in the autumn of 1935, because of the almost insurmountable prejudice in favor of dogfighting capabilities over all others among senior JNAF officers. The Ka-14’s low wing loading made it extremely maneuverable for a monoplane, but it still could not match the maneuverability of the A4N1—until the rules of mock combat were altered to include climb and dive tactics. That change gave the Ka-14 such an overall edge that even Minoru Genda, one of the most ardent biplane partisans, was won over to the new type.

After further development—and an unsuccessful attempt to interest the army in the design—Mitsubishi was able to put its monoplane into production as the A5M1 Model 96 carrier fighter in the autumn of 1936. An improved version with a 610-horsepower Kotobuki 2 KAI 3ko engine, a longer chord cowling, and a three-blade propeller in place of the two-blade airscrew entered production in the late spring of 1937 as the A5M2-ko. The outbreak of war with China on July 7, 1937, lent urgency to the JNAF’s efforts to hasten the A5M to operational units, and the newly formed 13th Kokutai (Air Group) got its first monoplanes just four days later.


“Battle of Shanghai”
Initially, the Japanese army advanced quickly, taking Beijing and Tientsin; but resistance stiffened as it approached Shanghai, and at the same time Japan’s regular arsenal of biplanes was proving unable to achieve a decisive degree of air superiority over the mixed bag of Chinese aircraft that opposed them. The need for such an edge became critical on August 14, when nine Mitsubishi G3M2s of the Kanoya Kokutai, led by Lt. Cmdr. Shinichi Nitta, left Matsuyama (Sung Shan) air base near Taipei, Taiwan, crossed the Formosa Strait and tried to bomb Jienqiao training field near Hangzhou, while another nine G3Ms led by Lt. Cmdr. Nantaro Asano attacked Guangde airfield. Chinese intelligence had learned of the coming mission and Colonel Kao Zihang, commander of the 4th Pursuit Group at Zhoujiakao, had ordered his 21st, 22nd, and 23rd Squadrons to Jienqiao, where their Curtiss Hawks would refuel and take off to intercept the raiders.

Kao’s fighters were the last of a long line of classic biplanes that had begun in 1925 with the P-1 Hawk (the first Curtiss to bear the name), and which culminated in the F11C-2 Goshawk. Final refinements in the Goshawk were metal wings and hand-cranked retractable landing gear on the XF11C-3, inspired by that of the Grumman XFF-1 two-seat fighter. Entering US Navy service in May 1933, the F11C-3—later redesignated as the BF2C-1 fighter-bomber—joined the Grumman F3F and Polikarpov I-153 as the only single-seat biplane fighters with retractable undercarriage to achieve quantity production.

Export versions of both Goshawk variants reverted to wooden wing structures, the fixed-gear plane being called the Hawk II and the retractable model the Hawk III. Powered by a 740-horsepower Wright R-1820-F53 radial engine, the Hawk III had a top speed of 240 miles per hour, mounted two .30-caliber Browning machine guns, and served in the air arms of Thailand and Argentina as well as China, which imported its first twelve in March 1936. Another ninety arrived in crates and were assembled at the Central Manufacturing Company at Hangzhou. The Chinese had seventy-two operational when the Japanese invaded, as well as fifty Hawk IIs.

August 14 began with Chinese air attacks against the Japanese army in Shanghai and against supporting naval units offshore, including Hawks of the 5th Pursuit Group carrying one 250-kilogram bomb each. Lieutenant Liang Hongwen in plane No. 2401 of the 24th Pursuit Squadron was credited with hitting the stern of the Japanese light cruiser Idzumo off Nantong, but it turned out to be a near miss—which was fortunate, since his target was in fact the British heavy cruiser Cumberland. Two other Chinese bombs fell near the American heavy cruiser Augusta. Another “international incident” occurred that afternoon when three Hawks from the 24th attacked the Japanese-occupied Kungda Textile Factory, but one of their bombs fell on the Nanking Road in the International Settlement. Meanwhile, Liang came under attack by an aggressively flown Nakajima E8N1 floatplane from the light cruiser Sendai, and was so badly shot about that he had to force land and died of his injuries soon after. Next, five Hawk IIs and nine Hawk IIIs made another attempt to bomb the Kungda factory, and some also attacked the floatplane, scoring fifteen hits before it lost them in a cloud.

Poor though the Chinese bombing performance was, it spurred Vice Adm. Kiyoshi Hasegawa, commander of the Japanese Third Fleet, to order attacks against their airfields. Due to typhoon weather conditions, however, the only unit game to defy them was the Kanoya Kokutai with its modern G3Ms—all-metal twin-engine monoplanes capable of 232 miles per hour and of mounting three 7.7mm machine guns. They took off at 1305 hours Formosa time, but storm clouds and poor visibility limited their altitude to 1,641 feet. They would also have to carry out their mission without fighter escort, but the Japanese were not overly concerned, arrogantly assuming that they would not need it against the inept Chinese.

The 4th Group’s Hawk IIIs were still in the process of refueling at Jienqiao when Nitto’s bombers arrived, strung out due to the weather, which made it hazardous to fly in formation. Kao, boarding his personal Hawk III marked IV-I, ordered all fighters to scramble up, ready or not. This had grave consequences for two of them—Hawk III 2105 of the 21st Pursuit Squadron ran out of fuel and crashed, mortally injuring Lt. Liu Shufan, and 2106 force landed, injuring Lt. Chin Anyi. The rest laid into the Japanese, and Colonel Kao, after silencing two gunners, closed to twenty meters to shoot a G3M, piloted by Petty Officer 3rd Class Iyoshio Momosaki, down in flames over Banshan. He then attacked Warrant Officer Fujio Yamashita’s bomber, crippling its left engine with fourteen hits, along with twenty-one in its right wing, and thirty-eight to the fuselage before his fuel gave out, compelling him to disengage and force land at Jienqiao. A third G3M, piloted by Petty Officer 1st Class Yanase Mitsui, and which was swarmed by 21st Squadron Hawk IIIs flown by Capt. Lee Guitan, Lt. Wang Wenhua, and Liu Chisheng, went down near Chiaosi.

At 1800 hours Asano’s nine G3Ms arrived over Guangde in V formation but only scored one bomb hit. As they made for home, they encountered Capt. Chow Tingfong, commander of the 34th Provisional Pursuit Squadron, who had been test-flying a Hawk III. Although he had no ammunition, Chow attacked and managed to break up the formation. As the Japanese flew on, they ran into the 22nd Pursuit Squadron, and one of its pilots, Lt. Cheng Hsiaoyu, hit the right engine and wing tank of Warrant Officer Hitoshi Ogawa’s G3M. Ogawa pressed on for Taiwan but ran out of fuel short of his goal and ditched near the Keelung harbor lighthouse, where he and his crew were rescued. Yamashita managed to get his riddled bomber back to Matsuyama on one engine, but its landing gear collapsed on landing, and it was written off.

Though overlooked in the West, the “Battle of Shanghai” had multiple significances in aviation annals. In 1940 the Republic of China pronounced August 14 as “Air Force Day.” Indeed, Colonel Kao had scored his air arm’s first aerial victories. To his shared kill that day, Liu Chisheng would add ten more flying Hawks, I-16s, and I-152s, to become China’s ace of aces and a major general in the Republic of China Air Force. In terms of air strategy, the Chinese fighters’ success struck a serious blow to Italian general Giulio Douhet’s widely accepted theory that bombers alone could win wars. Conversely, the Japanese were rudely awakened to the folly of sending their bombers in unescorted, and to the critical need for a fighter capable of seizing control of the sky.

Land-based Japanese navy units, augmented by the air groups of the light carrier Hosho off Shanghai, were joined on August 15 by the large carrier Kaga, and both vessels achieved a marginal degree of local air superiority with their aging Nakajima A2N1 fighters.