Focke-Wulf Ta 152

Focke-Wulf Ta 152

The Ta 152 entered Luftwaffe service in January 1945, with JG 301 as the only unit to operate it.

Designed as a high-altitude interceptor, it was rushed into service before all development issues were resolved.

Despite its exceptional performance—especially the Ta 152H variant—only around 43 to 69 aircraft were completed due to production delays and Germany’s collapsing war effort.

Ta 152s were primarily tasked with defending airfields and intercepting Allied reconnaissance and bomber aircraft.

Pilots reported excellent speed, climb rate, and manoeuvrability at altitude.

However, the aircraft saw limited combat and had no strategic impact on the war’s outcome.

After May 1945, the Ta 152 was retired, with no postwar use or export.

Its advanced design influenced later high-performance aircraft but remained a rare and short-lived operational type.

Prototypes & Development Airframes

These were experimental conversions or testbeds, often based on Fw 190D airframes

Ta 152 V1

Prototype converted from Fw 190 V32/U1; powered by Jumo 213A.

Ta 152 V2

Similar to V1;

used for aerodynamic testing.

Ta 152 V3

The first prototype had a pressurised cockpit and a Jumo 213E engine.

Ta 152 V4–V6

Continued development of the H-series: the V6 was the first with the full H-1 configuration.

Ta 152 V7–V10

C-series prototypes with DB 603 engines; the V7 was used for armament trials.

Ta 152 V11–V14

Further refinements:

V14 was a reconnaissance prototype (basis for E-series).

Ta 152 V15–V18

Late-war testbeds; V18 was reportedly a high-speed test aircraft.

Preproduction Series

These were limited-run aircraft used for evaluation and training

Ta 152 H-0

Preproduction high-altitude fighter: pressurised cockpit, long wingspan.

Ta 152 C-0

Preproduction medium-altitude fighter; shorter wings, DB 603 engine.

Ta 152 E-0

Reconnaissance variant; hybrid of H and C features, equipped with cameras.

Production Variants

Only a small number were completed before war’s end

Ta 152 H-1

High-altitude interceptor, the Jumo 213E, with ~25 built, saw limited combat in 1945.

Ta 152 C-1 

Medium-altitude fighter, DB 603LA, ~1–2 completed; not operational.

Ta 152 C-3

Improved C-series, DB 603L, possibly 1 built, and an armament upgrade.

Ta 152 E-1

Reconnaissance, Jumo 213E, unclear if completed.

Unbuilt or Paper Variants

These were planned but never constructed

Ta 152 H-10

Proposed reconnaissance version.

Ta 152 C-5

Ground-attack variant with additional armament.

Ta 152 R-series

Ramjet-assisted high-speed interceptors.

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 rounds

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

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