Initial design work was begun by Junkers in 1946, with the formal development contract being issued in the wake of the cancellation of the Heinkel P1068. A prototype is expected to fly in mid-1948.
Technical Data
Engines: Six Junkers 012 turbojet engines each rated at 3,000 kg (29.4 kN) thrust
Wingspan: 32.4 metres
Length: 30.8 metres
Height: 8.4 metres
Wing area: 161 square metres
Empty weight: 31,300 kg
Maximum permissible load: 65,000 kg
Maximum speed: 840 kph
Cruising speed: 475 kph
Rate of climb: 15.5 metres/second
Service ceiling: 12,500 metres
Range with maximum fuel load: 6,500 kilometres
Range with maximum war load: 4,000 kilometres
Defensive armament: two 20mm cannon in dorsal, ventral, and rear turrets, remotely controlled from cockpit
Offensive armament: Maximum bombload 5,000 kg