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				Possible constructed BMW Flugelrad 
				II V-2 in flight, April 1945Powered by underbody BMW 003 turbojets
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				Drawing by Richard Lewis Mendes 
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	by Rob Arndt 
	1943
 BMW Flugelrad I V-1 was painted matte aluminium and performed its first 
	flying test at the Czech Aerodrome at Prag-Kbely between August and 
	September. It left the hanger by its own means, the rotor began to spin and 
	the machine lifted to 1 meter and flew for 300 meters before making a hard 
	landing. During static tests the prototype was surrounded by concrete blocks 
	to protect the crew in the event of a disc blade breaking. In appearance the 
	basic Flugelrad lay-out was of a central body housing a pilot covered by a 
	hemispheric dome surrounded by a disc blade rotor of 6 meters with a lower 
	body housing a BMW 003 jet engine, fuel, a Strahlrohr jet deflector and 
	fixed landing gear of 4 legs fitted with wheels (with no brakes nor shock 
	absorbers). Flight was achieved by jet exhaust deflection into the 16 
	variable-pitch disc blades with hydropneumatic actuators.
 
 1944
 
 Several changes were introduced on the second prototype designated BMW Flugelrad I V-2. The cockpit was enlarged to carry two crew and serve as 
	support for the addition of an aerodynamic rudder. The fixed landing gear 
	was replaced with a more practical semi-retractable one. Rotor diameter was 
	enlarged to 8 meters but kept the 16 disc blades. The machine was painted 
	yellow and performed its first flight tests in the autumn of 1944 at the 
	Neubiberg Aerodrome near BMW's Munich facility. Stability problems continued 
	to plague the machine.
 
 1945
 
 The next prototype, BMW Flugelrad II V-1, kept the same body but discarded 
	the failed rudder, which proved almost useless. The rotor was enlarged to 
	12.6 meters. The first flight was at Prag-Kbely in February 1945 with 
	another jump at low altitude. Three other Flugelrad models were under study 
	in early 1945:
 
		
			
			
			the BMW Flugelrad II V-2 under construction
			
			the BMW Flugelrad II V-3 models
			
			the BMW Flugelrad III design phase 
	Both the 
	BMW Flugelrads II V-2 and V-3 would have used two BMW 003 engines in the 
	lower body side-by-side, enlarged cockpits for four crew, and rotor 
	enlargement to 14.4 meters (although the V-2 would have had 24 disc blades 
	while the V-3 would have had 21). The final BMW Flugelrad III would have 
	been the production aircraft- a huge stratospheric recon aircraft powered by 
	two BMW 018 engines each with twin Strahlrohrs mounted one above the other, 
	an upper and lower cockpit arrangement, 6 crew, enlarged 24 meter rotor with 
	32 disc blades, fully retractable gear, and room for an array of recon 
	cameras. Nevertheless, all work ceased on the Flugelrads in April 1945. All 
	prototypes and documentation were destroyed in the Russian advance.
 
	
	 
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