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Fw 190 D-9 (“Dora”) — Summary

1. Overview

Derivative: A long-nose derivative of Fw 190A (air-cooled) fitted with the liquid-cooled V-12 Jumo 213A-1 (“Dora”). Main intent of modifications: Adoption of an annular radiator to limit drag increase while concentrating structural changes mainly in the nose section. First flight: September 1942. Production & service: Mass production from Aug 1944 → frontline allocation in Nov → combat use from Dec. High-altitude suitability: Turbo-supercharger and cockpit pressurization ultimately not adopted. While it avoided the sharp high-altitude power drop seen on the A-series, the D-9 was fielded as a transitional high-speed fighter.

2. Airframe & Propulsion

Engine: Jumo 213A-1 (liquid-cooled V-12) with MW50 (10 minutes continuous per use, 40 minutes total). Overall length: 8.95 m → 10.192 m (nose approx. +50 cm, rear fuselage approx. +49 cm). Empennage: Enlarged vertical tail (for stability). Intake: Supercharger intake protruding on the starboard nose. Cooling: Annular radiator mounted ahead of the engine. Pressurization: No pressurized cockpit in the final configuration. Turbo: No turbo-supercharger.

3. Engine Power

Condition / Altitude Power (hp)
Takeoff (rating) 1,776
5,800 m 1,600
With MW50 (10 min / 40 min total) ~2,240
9,800 m ~1,020

4. Performance

Item Condition Figure
Maximum speed at 6,400 m 698 km/h
Maximum speed (MW50) at 6,200 m with MW50 732 km/h
Service ceiling 13,200 m

5. Handling / Armament / Equipment

Handling: Roll performance decreased as the price for higher speed; however, pilot evaluations were generally favorable after familiarization. Fixed armament:

Nose: MG 131 13 mm × 2 (475 rpg)

Inboard wings: MG 151/20 20 mm × 2 (250 rpg) Protection: 12 mm armor plate behind the pilot / 50 mm armored windscreen in front. Ordnance: ETC501 / ETC504 centerline rack for bombs. Canopy: About 300 early aircraft retained the earlier canopy; later machines adopted the “Galland” blown canopy for better visibility. All-weather variant R11 (operational contribution: ○): canopy de-icing, FuG 125 radio navigation/landing guidance, LGWK 23 course indicator, PKS 12 autopilot. Other planned sub-variants saw little or no operational use.

6. Production & Allocation

Category Figures / Notes
D-9 + D-9/R11 ~750 aircraft (per some sources)
D-series total 1,805 aircraft (per some sources)
D-9 only 1,826 produced, but ~300 said to have seen combat (per another account)

(Notes) Figures vary by scope definitions (D-9 only vs. entire D-series; completed vs. accepted vs. operational). When citing, specify the coverage and basis of each number.

7. Operational Assessment (Highlights)

Background: Bombing of BMW plants depressed A-series output → D-9 brought forward into mass production. Combat: Entered combat by Dec 1944, but the Luftwaffe fighter arm suffered heavy losses during the “Wacht am Rhein” (Ardennes) offensive that month. Overall judgment: The airframe possessed credible potential against late-war Allied fighters, yet the lack of seasoned pilots and overwhelming material inferiority meant it could not alter the strategic picture. Designer’s view: For Kurt Tank, the D-series was a stopgap, with Ta 152 as the true objective. Anecdotally, voicing this view hurt unit morale.

8. Comparative Assessments

Nohara & Shiwaku (1990); Nohara (2003): Emphasize aerodynamic refinement, the annular radiator’s advantages, and power superiority (approx. 1,750 hp for D-9 vs. ~1,450 hp for P-51), suggesting that in pure dogfight terms the D-9 could surpass the P-51. Rekishi-Gunzō (2010): While German sources rated the D-9 as comparable to the P-51D, much published data rely on estimated figures, and actual performance may have been slightly inferior to the latest Allied types.

9. Timeline (Concise)

Date Event
Sep 1942 First flight
Late Jun 1944 Two prototypes completed
Aug 1944 D-9 mass production begins
Nov 1944 Frontline allocation begins
Dec 1944 Combat debut (coinciding with the Wacht am Rhein / Ardennes period)

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