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Origin: Focke-Wulf Flugzeugbau GmbH Type: Single-seat high altitude fighter Models: Ta 152C & H Crew: One First Flight: N/A Service Delivery: N/A Total Production: N/A POWERPLANT: Model: Junkers Jumo 213E-1 Number: One Type: 12-cylinder inverted Vee,liquid cooled with MW-50 injection and GM-1 boosting Horsepower: Take-Off: 1,750 hp at 3,250 RPM (2,050 hp w. MW 50) Climb And Combat: 1,580 hp at 3,000 RPM Maximum: 1,320 hp at 32,810 ft. (1,740 hp with GM 1 boost) Propeller Unit: Junkers wooden three blade unit Diameter: 3.6 m (11 ft. 9.75 in.) FLUID: Fuel: Capacity: 364 Imperial Gallons (1618 liters) Type: B4 (87 Octane) Oil: Capacity: 72 liters GM-1 (Nitrous Oxide): Capacity: 85 liters MW-50 (Methanol-Water) Capacity: 140 liters DIMENSIONS: Wing Span: 14.5m (47 ft. 6¾ in.) Wing Area: 23.5m² (252.95 Sq. Ft.) Length: 10.8m (35ft 5¼ in.) Height: 4m (13 ft. 1.5 in.) Wheel Track: 3.95m (12 ft. 11 in.) Stabilizer Span: N/A |
WEIGHTS: Empty: 3,600kg (7,940 lbs.) Loaded: 5,500kg (12,125 lbs.) PERFORMANCE: Maximum speed: 695km/h (431mph) at 10,500m (34,451 ft.) 750km/h (466mph) at 9,000m (29,529 ft.) with MW-50 760km/h (472mph) at 12,500m (41,012 ft.) with MW-50 and GM-1
Climb rate: 1000m/minute
ARMAMENTS:
Two inboard wing mounted 20mm MG151/20 (Occasionally outboard MG 151/20s as well, depending on model, some reconaissance models were unarmed) Bomb load: None
AVIONICS:
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