Focke-Wulf (Tank) Ta-152H
| GENERAL DATA | |||
| Other Designation(s) | - |
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| Type | High-Altitude
Fighter |
Crew | 1 |
| Manufacturer(s) | Focke Wulf Flugzeugbau
GmbH |
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| Production | 220; Ta-152B: 3, Ta-152B: prototypes, Ta-152E: 1, Ta-152H-0: 20, Ta-152H-1: 190 |
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| Prototype first flight | Late 1942, october 1944 (for H-0), november 1944 (for H-1) |
Introduction | 1944 |
| Variants | |||
| Ta-152A | Pressurized cabin. | ||
| Ta-152B | Pressurized cabin. Normal wing span. | ||
| Ta-152C-0 | Pre-production aircraft, 1 prototype built[5][page needed] powered with 2100-hp Daimler Benz DB603LA engine. The extra length of this engine, as with the Jumo 213-powered Fw 190D-9, required a compensating rear fuselage plug and enlarged tail surfaces, and wing span was increased to 11 meters. | ||
| Ta-152C-1 | Standard wing (11.00 m), armed with one engine-mounted Motorkanone 30 mm (1.18 in) MK 108 cannon and four 20 mm synchronized MG 151/20 cannons (two above the engine, two in the wing roots). | ||
| Ta-152C-2 | Standard wing (11.00 m), equipped with an improved radio. | ||
| Ta-152C-3 | Standard wing (11.00 m), armed with one engine-mounted Motorkanone 30 mm (1.18 in) MK 103 cannon and four 20 mm synchronized MG 151/20 cannons (two above the engine, two in the wing roots). | ||
| Ta-152E-1 | Photographic reconnaissance version of the Ta 152C, with standard wing (11.00 m) | ||
| Ta-152E-2 | High-altitude photographic reconnaissance version, powered by a Junkers Jumo 213E engine and with the H-series wing (14.44 m). Only a single prototype was completed. | ||
| Ta-152H-0 | 20 pre-production aircraft,
H-series wing (14.44 m) |
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| Ta-152H-1 | Only production version. H-series wing (14.44 m), armed with one engine-mounted Motorkanone 30 mm (1.18 in) MK108 cannon and two 20 mm synchronized MG 151/20 cannons in the wing roots, additional fuel tanks located in the wings. | ||
| Ta-152S | Two seat trainer. | ||
| DIMENSIONS (Ta-152H-1) | |||
| Empty Weight | 4031 kg |
Loaded Weight | 4727 kg |
| Max takeoff weight | 5217 kg |
Length | 10.82 m |
| Wingspan | 14.44 m |
Wing area | 23.5 m² |
| Height | 3,36 m |
Wing loading | 196.8 kg/m² |
| ARMAMENT (Ta-152H-1) | ||||
| Main Gun | Propeller | 1 × 30 mm MK 108 cannon |
Ammunition Carried |
85 |
| Secondary Guns | Wings | 2 × 20 mm MG 151/20 cannons |
Ammunition Carried | 2 x 175 |
| Bombs | - |
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| Rockets | - |
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| POWERPLANT (Ta-152H-1) | |||
| Engine | 1 ×
Jumo 213E |
Type & Displacement | 12-cylinder inverted
Vee, 35 L |
| Horsepower (maximum) | 1750-2050
hp* |
Power/Weight Ratio | 488-520 hp / ton ** |
| Fuel Capacity | 524
L plus provision for 115 L of auxiliary fuel in a rear-fuselage
tank (internal) + 1 x 300 L (80 US gal) drop tank
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(*) with GM-1 boost, (**) with loaded weight
| PERFORMANCES (Ta-152H-1) | |||
| Maximum Speed | 759 km/h
at 12500 m using GM-1 boost |
Cruise Speed | 500 km/h |
| Stall Speed * | ? km/h |
Service Ceiling | 15100 m using GM-1 boost |
| Rate of Climb | 20 m/s to 25.4 m/s |
Range | 1215 km , 2000 km with drop tanks |
(*) vitesse de décrochage
| Sources | |||
| Wikipédia | Lemaire Soft | ||
Drawings |
