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         In retrospect the Me 
         163 need not have suffered from its most serious faults, and the 263 
         emerged on the Lippisch/Messerschmitt drawing boards in winter 1943-44 
         to rectify them. The new design had larger and better shaped body 
         housing more propellants, a new engine with a separate low thrust 
         cruise chamber for long endurance, and a proper retractable landing 
         gear. The 163D V1 was completed in spring 1944 but the RLM transferred 
         the program to Junkers to ease Messerschmitt's production burdens. At 
         Dessau Prof Hertal improved the 263A-1 into the Ju 248, with automatic 
         slats, a bubble hood and a cut-down rear fuselage, larger flaps and 
         other changes. Two 30 mm MK 108 cannon were fitted in the wing roots as 
         the standard armament. The RLM insisted on restoration of the Me 263A-1 
         designation, and hastened production, planning for the use of the 5,511 
         lbs (2500 kg) BMW 708 nitric-acid motor when ready, but in the chaos of 
         late 1944 tooling was never finished, although a single Dessau built 
         263A-1 flew as a glider in 1944. It was developed by the Soviets but 
         they soon abandoned the project.   
         
           
         Specifications 
         (Messerschmitt Me 263 / Junkers Ju 248) 
         Type: Single 
         Seat Interceptor 
         Design: Dr 
         Alexander Lippisch  
         Manufacturer: 
         Messerschmitt AG (Later transferred to Junkers) 
         Powerplant: One 
         main chamber 3,750 hp (1700 kW / 16.67 kN) thrust Walter HWK 109-509C-4 
         bi-liquid propellant rocket motor burning concentrated hydrogen 
         peroxide (T-stoff) and hydrazine/methanol (C-stoff) and a 660 lbs (300 
         kg / 2.94 kN) cruise chamber. 
         Performance: 
         Maximum speed 620 mph (1000 km/h) at height; time to 49,231 ft (15000 
         m) about 3 minutes. 
         Range: Maximum 
         endurance, about 1 hour including 15 minutes under main power. 
         Weight: Empty 
         4,640 lbs (2105 kg) with a loaded take-off weight of 11,354 lbs (5150 
         kg). 
         Dimensions: Span 
         31 ft 2 in (9.50 m); length 25 ft 10.5 in (7.88 m); height 8 ft 10.25 
         in (2.70 m). 
         Armament: Two 30 
         mm MK 108 cannon with 60 rounds each mounted in the wing roots. 
         Variants: Me 
         163D (one aircraft only), Me 263A/A-1, Junkers Ju 248. 
         Avionics: None. 
         History: (Me 
         163D V-1) spring 1944; (Me 263A-1) flew as a glider in August 1944. 
         Operators: 
         Germany (Luftwaffe).   |