Gotha WD.7

Last updated
WD.7 and WD.8
Gotha WD.7 on beaching trolleys.jpg
A forward oblique view of a WD.7 on its beaching trolleys
Role Maritime reconnaissance aircraft and torpedo-bomber trainer
National originGermany
Manufacturer Gothaer Waggonfabrik
First flightDecember 1915
Primary user Imperial German Navy
Number built8 x WD.7; 1 x WD.8

The Gotha WD.7 (Wasser Doppeldecker - "Water Biplane") was a twin-engine maritime patrol and torpedo-bomber training floatplane developed during World War I by Gothaer Waggonfabrik for the Imperial German Navy's (Kaiserliche Marine) Naval Air Service (Marine-Fliegerabteilung). The WD.8 was a single-engine version of the WD.7 developed for comparative purposes. The single aircraft built was deemed "totally unsuitable" by the Naval Air Service and was later sold to the Ottoman Empire.

Contents

Development

After the submarine SM U-9 sank three British armored cruisers on 22 September 1914 shortly after the war began, the German Imperial Naval Office (Reichsmarine-Amt) decided to try mounting torpedoes on aircraft as they were far easier and faster to build than submarines. Early trials with land-based aircraft were unsuccessful because of the great weight of the torpedo (645 kilograms (1,422 lb)) was more than existing aircraft could easily lift and the danger of trying to fly from an uneven grass airstrip with such a large weight of explosives. At the beginning of 1915 the Naval Office ordered the development of seaplanes capable of carrying torpedoes and the Seaplane Experimental Command (Seeflugzeug-Versuchs-Kommando (SVK)) issued requirements for these aircraft. They had to be twin-engine airplanes armed with a machine gun for self-defense and with a crew of two or three men: a pilot and observer for torpedo missions and a pilot, bombardier and gunner for bombing missions. [1]

Even before the pusher-configuration WD.3 was rejected by the SVK in late 1915, [2] Gotha turned to a new layout that would also keep the aircraft's nose free for forward-firing weapons. The WD.7 was a tractor-configuration biplane with 120- horsepower (89  kW ) Mercedes D.II straight-six engines mounted on the leading edge of the lower wing. The radiators were located above each engine. The aircraft did retain the WD.3's nose and gunner's cockpit in addition to the twin-tail tail structure. The prototype kept the central vertical stabilizer as well, but this was eliminated in the production aircraft. [3]

Eight examples were built for use as trainers for torpedo bombing. During 1917, two of these aircraft were used for testing a 37 mm (1.46 in) autocannon built by DWM and the Becker 20 mm (0.8 in) autocannon.

Gotha WD.8 Gotha WD.8.jpg
Gotha WD.8

The same airframe was used to create the WD.8 reconnaissance floatplane, substituting the two wing-mounted engines with a single water-cooled 240-horsepower (180 kW) Maybach Mb.IVa straight-six engine in the nose.


Variants

WD.7
twin-engine torpedo bomber trainer floatplane, powered by two 120 hp (89 kW) Mercedes D.II. [4]
WD.8
single-engine reconnaissance floatplane, powered by a 240 hp (180 kW) Maybach Mb.IV. [4]

Specifications (WD.7 prototype)

Gotha WD.7 3-view drawing from Aviation and Aeronautical Engineering September 15, 1916 Gotha WD.7 3-view Aviation and Aeronautical Engineering September 15,1916.png
Gotha WD.7 3-view drawing from Aviation and Aeronautical Engineering September 15, 1916

Data from Gotha Aircraft of WWI: A Centennial Perspective on Great War Airplanes; [5] German Aircraft of the First World War [4]

General characteristics

WD.8: 11.2 m (37 ft)
WD.8: 16 m (52 ft)
WD.8: 4.1 m (13 ft)
WD.8: 1,254 kg (2,765 lb)
WD.8: 1,778 kg (3,920 lb)

Performance

WD.8: 138 km/h (86 mph; 75 kn)
WD.8: 480 km (300 mi)
WD.8: 4,500 m (14,800 ft)
  • 40 minutes to 2,000 m (6,600 ft)
WD.8: 6.5 minutes to 1000 m
  • 25 minutes to 2,500 m (8,200 ft)

Armament

WD.8: 1 x 7.62 mm Parabellum MG 14 machine gun in the rear cockpit

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References

  1. Schmeelke, pp. 3, 10
  2. Herris, p. 36
  3. Nowarra, Robertson & Cooksley, p. 44
  4. 1 2 3 Gray & Thetford, p. 400
  5. Herris, pp. 45, 48

Bibliography