Focke-Wulf Ta 153

From Wikipedia, the free encyclopedia

The Focke-Wulf Ta 153 (GH+KV) was a prototype German fighter aircraft built during World War II. It was a development of the Focke-Wulf Ta 152 with long-span, high-aspect ratio wings. The prototype never flew because the German factory it was being built in was overrun.

[edit] Specifications (Ta 153)

[edit] General characteristics

  • Crew: one, pilot
  • Length: 10.40 m (34 ft 1 in)
  • Wingspan: 11.00 m (36 ft 1 in)
  • Height: 3.40 m (11 ft 2 in)
  • Wing area: 18.2 m² (196 ft²)
  • Empty: 3,600 kg (7,937 lb)
  • Loaded: 4,400 kg (9,700 lb)
  • Maximum takeoff: 5,100 kg (11,244 lb)
  • Powerplant:Junkers Jumo 213, 1,305 kW (1,750 hp)

[edit] Performance

  • Maximum speed: 680 km/h (424 mph)
  • Range: 1,400 km (873 miles)
  • Service ceiling: 11,000 m (36,080 ft)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: 242 kg/m² (50 lb/ft²)
  • Power/mass: 0.30 kW/kg (0.18 hp/lb)

[edit] Armament

[edit] Related content

Related development: Focke-Wulf Fw 190 - Focke-Wulf Ta 152

Comparable aircraft:

Designation sequence: Go 150 - Kl 151 - Ta 152/Kl 152 - Ta 153 - Ta 154 - BV 155 - Fi 156