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Messerschmitt Me 263




  type Interceptor fighter
  manufacturer Messerschmitt / Junkers
  designer Alexander Lippisch
  first Flight August 1944 (Unpowered)
  primary User Luftwaffe
  number Built 1
  developed From Messerschmitt Me 163


For the fictional aircraft of this designation from


The Messerschmitt Me 263 was a Rocket -powered Fighter Aircraft developed from the Messerschmitt Me 163 towards the end of World War II . Only one prototype was built as the rapidly deteriorating military situation in Germany prevented the completion of further aircraft.

Early in the project's life, the aircraft was redesignated the Junkers Ju 248 resulting from the complicated nature of the later developments of the Me 163. After the original designer, Alexander Lippisch left the project, Junkers was put in charge of finishing development of the Me 163D variant and was issued a new designation for the type.

The aircraft was an attempt to overcome the largest shortcomings of the Me 163B, based on the results of tests with the Me 163D (sometimes referred to as the '''Me 263 V1'''). The fuselage was considerably modified to accommodate larger fuel tanks to give longer range, the cockpit was redesigned for pressurization and fitted with a Bubble Canopy to improve the rear view for the pilot, and the Me 163's skid undercarriage was replaced with a conventional retractable Undercarriage . The Walter rocket engine was modified to have two chambers - a main chamber to provide power for takeoff and climb, and an auxiliary chamber to provide lower power (and therefore lower fuel consumption) for cruising at altitude. The auxiliary chamber afforded a thrust of 300 kg (660 lb) which was in addition to the main chamber's normal thrust of 1,700 kg (3,750 lb), and the intention was that the aircraft should take off and climb to operational altitude with both rocket chambers operating at full thrust, then cut the main chamber and cruise on the power of the auxiliary chamber alone. This engine arrangement had previously been tested on modified Me 163Bs. By early August 1944 , the prototype was undergoing glide tests, towed aloft by a Junkers Ju 188 . Apparently, the Walter engine was fitted in September, but it is not clear if the aircraft was ever tested under power. In late September, the aircraft was ordered into production.

In early 1945 , the RLM re-assigned the project to Messerschmitt, and re-instated the Me 263 designation, but the aircraft never reached the production line. The production version was intended to be powered by the more powerful BMW 708 rocket engine in place of the Walter powerplant. In the meantime, the Junkers factory was overrun by the Red Army and the prototype Ju 248, along with materials and staff, were captured and taken to the Soviet Union .

Further development of the design continued after the war, resulting in the abortive Mikoyan-Gurevich I-270 interceptor.


DEVELOPMENT SEQUENCE



SPECIFICATIONS (ME 263 V1)

  plane Or Copter plane
  jet Or Prop jet
  crew 1
  length Main 789 m
  length Alt 25 ft 10⅔ in
  span Main 950 m
  span Alt 31 ft 2 in
  height Main 269 m
  height Alt 8 ft 10¼ in
  area Main 1780 m&2
  area Alt 19159 ft&2
  empty Weight Main 2,105 kg
  empty Weight Alt 4,640 lb
  max Takeoff Weight Main 5,150 kg
  max Takeoff Weight Alt 11,354 lb
  engine (jet) Walter HWK 109-509 C-4
  type Of Jet rocket
  number Of Jets 1
  thrust Main 1961 kN
  thrust Alt 4,410 lb
  max Speed Main 997 km/h
  max Speed Alt 620 mph
  ceiling Main 15,000 m
  ceiling Alt 49,212 ft
  climb Rate Main 5,000 m/min
  climb Rate Alt 16,404 ft/min




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