I-270, Me 163 and Ju 248 / Me 263 Performance Comparison

Via Eric Bond

This table is for purposes of comparing similarities and differences among designs. By no means should this be used to draw unsubstantiated conclusions, for example, Aircraft A is a copy of Aircraft B, or Aircraft X is better than Aircraft Y. Some performance figures given may not be attainable under certain circumstances, for example, Aircraft A's top speed may be in a clean (no warload) configuration, while Aircraft B's top speed may be at a different altitude, with a full load.

I-270 Me 163B-1a Ju 248 / Me 263 Power (total thrust): 3,197 lb ( 1,450 kg) 3,750 lb (1,700 kg) 5,292 lb (2,400 kg) Loaded weight: 9,083 lb (4,120 kg) 9,502 lb (4,310 kg) 11,684 lb (5,300 kg) Max speed: 582 mph @ 49,215 ft 593 mph @ 9,850 - 29,500 ft 547 mph @ 10,000 - 36,090 ft (est.)   936 kph @ 15,000 m 955 kph @ 3,000 - 9,000 m 880 kph @ 3,050 - 11,000 m (est.) Max endurance: 9.05 min 22 miles (35.5 km) (combat radius) 14.75 min Armament: 2 x 23 mm cannon 2 x 30 mm cannon 2 x 30 mm cannon   8 x RS-82 rockets

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I-270

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