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         August 11, 1945 -- an excellent side-elevation view of the first 
         prototype Kikka; note the strong resemblance to the Me 262.
          
         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.  
         
           
         Last-minute adjustments are made to the Kikka's starboard engine 
          
         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.  
         
           
         The Kikka's Ne-20 turbojet engine  
         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.  
         
           
         The Kikka's test pilot and a ground crewman look on as a technician 
         makes sure all systems are 'Go'.  
         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. 
          
         
           
         The second prototype Kikka, seen just after the close of the war 
          
         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.   |