Messerschmitt Me 209 V1 (Huma Models)

TYPE: Racing aircraft

ACCOMMODATION: Pilot only

POWER PLANT: One Daimler-Benz DB 601 ARJ liquid-cooled engine, rated at 1,775 hp

PERFORMANCE: 469 mph

COMMENT: The Messerschmitt Me 209 V1 was a single-engine racing aircraft which was designed for and succeeded at breaking speed records.
The designation Me 209 was used for two separate projects during World War II. The first was a record-setting, single-engined race aircraft, for which little or no consideration was given to adaptation for combat. The second Me 209  V4 was a proposal for a follow-up to the highly successful Messerschmitt Bf 109 which served as the Luftwaffe’s primary fighter throughout World War II.
Designed in 1937, the Me 209 V1 was a completely separate aircraft from the Messerschmitt Bf 109, solely designed to break speed records. It shared only its Daimler-Benz DB 601 engine with the Bf 109, which in the Me 209 was equipped with steam cooling. Willy Messerschmitt designed the small aircraft with a cockpit placed far back along the fuselage just in front of its unique cross-shaped tail section. Unlike the Bf 109, the Me 209 featured a wide track, inwardly-retracting undercarriage mounted in the wing section.
The aircraft achieved its purpose when test pilot Fritz Wendel flew it to a new world speed record of almost 469 mph on 26 April 1939, bearing the German civil registration D-INJR. This record was not officially broken by another piston-engined aircraft until 16 August 1969 by Darry Greenamyer’s highly modified Conquest F8F “Bearcat”.
The Me 209 V1’s speed record was itself shattered in terms of absolute speed, eighteen months later by Heini Dittmar, flying another Messerschmitt aircraft design, the Messerschmitt Me 163A V4 rocket fighter prototype to a 624 mph record in October 1941.
The idea of adapting the Messerschmitt Me 209 racer to the fighter role gained momentum when, during the Battle of Britain, the Messerschmitt Bf (Me)109 failed to gain superiority over the Royal Air Force’s Supermarine “Spitfire”. The little record-setter, however, was not up to the task of air combat. Its wings were almost completely occupied by the engine’s liquid cooling system and therefore prohibited conventional installation of armament. The aircraft also proved difficult to fly and extremely hard to control on the ground. Nevertheless, the Messerschmitt team made several attempts to improve the aircraft’s performance by giving it longer wings, a taller vertical stabilizer, and installing two synchronized 7.92 mm MG 17 in the engine cowling. Several modifications on the aircraft, designated Messerschmitt Me 209 V4, however, added so much weight that the aircraft ended up slower than the contemporary Bf 109E. As a result the complete Messerschmitt Me 209 project was soon cancelled, but was revived later in form of the Messerschmitt Me 209 V5. (Ref.: 24).

Kokukyoko “Syusuishiki Kayaku ”, (“Autumn Water”), Unicraft Models, Resin

TYPE: Rammer aircraft

ACCOMMODATION: Pilot only

POWER PLANT: Four Type 4 Mk. 1 Model 20 solid fuel rockets with a combined 1,102 kp thrust

PERFORMANCE: 699 mph (estimated)

COMMENT: The practice of ramming, in Japanese “tai-atari”, which literally means “body crashing”, was not unique to Japan. During WW II the deliberate ramming of one aircraft by another aircraft was performed by the Russians, Germans as well as Japanese and all made ramming a part of their war doctrine.
The Japanese would use aircraft already in operational service for ramming attacks such as that Kawasaki Ki-45 and even stripped down Kawasaki Ki-61 “Hein” fighters. It was long thought that Japan never developed a dedicated rammer aircraft of its own but this is no longer the case. Recently discovered in the archives of the Japanese National Institute for Defense Studies is just such a project.
The aircraft was a joint venture between the Imperial Japanese Army (IJA) and the Imperial Japanese Navy (IJN), something that occurred with more regularity towards the closing stage of WW II. The design was based on the “Syusuishiki Kayaku” Rocketto (“Autumn Water”-type ram attack rocket), a project started in March 1945 for an unmanned, remote controlled anti-bomber missile. The plan was to ground launch the missile, guide it remotely towards the target, engage the target via ramming, and then recover the missile (if it survived the collision) for reuse.
Design work was carried out by the Kokukyoko (the Aeronautical Bureau) and, although a mockup was completed, the war ended before finalized production plans could be completed, let alone the missile ever being tested.
The piloted version used much the same design as the missile and was a small, tailless aircraft featuring low mounted 45′ swept wings. The fuselage was bullet shaped with a large vertical stabilizer into which the cockpit was blended. Located in the back of the fuselage were four Type 4 Mark 1 Model 20 rockets, the same as those used on the Kugisho MXYT “Oka” which on such a small aircraft pushed the maximum speed to an estimated 699 mph or just over Mach 0.91. lt is unknown if the design had swept wings because the designers  understood the principles in relation to overcoming compressibility problem at transonic speeds, or if the shape was chosen as a means to provide an angled cutting surface to facilitate ramming attacks, or as a drag reducing planform. The wings were strengthened to withstand the high impact forces experienced when striking the enemy bomber. Even though the rammer could rely on speed as a defense when under power, it still had to contend with the defensive armament of the B-29 and thought the pilot had some measure of armor plating and bulletproof glass to protect him. The aircraft was certainly capable of gliding back to base to be refueled and relaunched once it had conducted its attacks. Given the small size of the plane, no landing gear was fitted. As such, it is likely the underside of the fuselage was reinforced or had a skid installed. How it was to be launched is unknown – it could have been towed aloft, catapult launched or perhaps even vertically launched.
In a ram attack, typically the tail would be targeted because the loss of the tail assembly would send the bomber out of control. Striking the wings and engines was another focus of ramming attacks. Finally, the aircraft fuselage was the other key area to strike. The probable mission profile of the rammer flying from a ground base would include being positioned within very close proximity of likely bombing targets. With the short burn time of the rockets (8-10 seconds) the aircraft’s operational radius would have been very limited. After launching, as bombers came into range the pilot would attempt to ram into either the tail or wing of the target with the objective of severing it from the fuselage. If enough speed momentum remained after the initial hit, another ram attack would be made. Should the aircraft remain in flying condition and if the pilot did not elect to ram his entire plane into a target, he would return to base where the rockets would be replaced. If the bombers were still close by, he could fly another sortie. If the rammer was towed into the air, the rockets would most likely have been fired on approach and again after hitting a target. This would provide enough power to grant a second pass with sufficient speed to allow for significant damage to be inflicted on the bomber when it struck.
However, the Kokukyoko “Syusuishiki Kayaku” would remain a paper project only. It is unclear if the design was to be the definitive rammer model or simply a proposed concept (Ref.: Dyer III, Edwin M.: Japanese Secret Projects, Experimental Aircraft of the IJA and IJN 1939-1945, Midland Publishing, Hersham, U.K., 2010).