Focke-Wulf Ta 152

The Focke-Wulf Ta 152 is a German fighter and interceptor aircraft designed for high-altitude operations by Kurt Tank and manufactured by Focke-Wulf.

Unfortunately, it began production too late and in inadequate quantities to play a meaningful role in the Second World War.

The Ta 152 was an evolution of the Focke-Wulf Fw 190 fighter.

It was planned to be available in at least three variants:

The Ta 152H Höhenjäger (high-altitude fighter);

The Ta 152C, which was tailored for medium-altitude missions and ground-attack, featuring a Daimler-Benz DB 603 engine and smaller wings;

The Ta 152E, a fighter-reconnaissance model that combined the engine of the H variant with the wings of the C variant.

The initial Ta 152H was introduced into service with the Luftwaffe in January 1945; however, production of the Ta 152 was halted just one month later due to Germany’s deteriorating situation in the war.

Japan sought to obtain materials from Germany to initiate domestic production of the Ta 152, but it is believed that no aircraft were ever completed.

By October 1944, in light of the disastrous trajectory of the conflict, the RLM recognised the critical nature of Germany’s predicament and urged Focke-Wulf to expedite the production of the Ta 152.

Consequently, several prototypes of the Ta 152 experienced crashes early in the testing phase.

It became evident that essential systems were not subjected to adequate quality control Issues emerged with superchargers, pressurised cockpits exhibited leaks, and the engine cooling system proved to be unreliable, partly due to inconsistent oil temperature monitoring.

Additionally, there were multiple instances where the landing gear failed to retract properly.

From November 1944, a total of up to 20 pre-production Ta 152 H-0s were supplied to Erprobungskommando Ta 152 for service testing of the aircraft.

Reports indicated that test pilots managed to accumulate only 31 hours of flight testing prior to the commencement of full production.

By the end of January 1945, approximately 50 hours of flight time had been logged.

The Ta 152’s tally at the conclusion of the war was likely seven victories and four losses in aerial engagements, although there remains some uncertainty regarding these figures.

Josef Keil secured four victories between 1 March 1945 and 21 April 1945, while at least three victories were credited to Willi Reschke.

The Ta 152 was assigned to JG 301 on 27 January 1945, with its inaugural mission against American bombers occurring on 2 March 1945.

However, there was no engagement with American forces, as the 12 Ta 152s had to defend against continuous assaults from the Bf 109s of a different German unit, given that the design of the Ta 152 was largely unfamiliar to other Jagdgeschwader.

Fortunately, there were no losses, as the climbing performance and agility of the Ta 152s allowed them to avoid these confrontations.

The four losses in aerial combat included Hptm. Hermann Stahl, who was killed on 11 April 1945;

Obfw. Sepp Sattler, who died on 14 April 1945;

and two unidentified JG11 pilots who were shot down by Spitfires in the final days of April 1945 while being transferred from Neustadt-Glewe to Leck airfield.

Specifications

Crew

one

Length

10.82 m (35 ft 6 in)

Wingspan

14.44 m (47 ft 5 in)

Height

3.36 m (11 ft 0 in)

Wing area

23.5 m² (253 sq ft)

Airfoil

Root

NACA 23015.3

Tip

NACA 23009

Empty weight

3,877 kg (8,547 lb)

Gross weight

5,217 kg (11,502 lb)

Max takeoff weight

5,217 kg (11,502 lb)

Fuel capacity

992 L (262 US gal; 218 imp gal)

Powerplant

1 × Junkers Jumo 213E or Junkers Jumo 213E-1 V-12 inverted liquid-cooled piston engine,

1,287 kW (1,726 hp) for take-off

1,530 kW (2,050 hp) for take-off with MW-50 water/methanol injection

940 kW (1,260 hp) at 10,700 m (35,100 ft) with GM-1 Nitrous Oxide injection

Propellers

3-bladed Junkers VS-9 constant-speed propeller

Performance

Maximum speed

580 km/h (360 mph, 310 kn) at sea level with MW-50 boost

759 km/h (472 mph; 410 kn) at 12,500 m (41,000 ft) with GM-1 boost

Range

2,000 km (1,200 mi, 1,100 nmi)

Service ceiling

15,100 m (49,500 ft) with GM-1 boost

Rate of climb

20 m/s (3,900 ft/min) at maximum weight of 5,217 kg (11,502 lb)

25.4 m/s (83 ft/s) at 4,727 kg (10,421 lb)

Time to altitude

10,000 m (33,000 ft) in ten minutes and six seconds

Wing loading

196.8 kg/m² (40.3 lb/sq ft)

Power/mass

0.276 kW/kg (0.168 hp/lb)

Armament

1 × 30 mm (1.181 in) MK 108 cannon 85 rds

2 × 20 mm (0.787 in) MG 151/20 cannon 350 rds.

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