Draft:Goebel Goe II
WWI German rotary aircraft engine
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Submission declined on 23 August 2025 by MediaKyle (talk).
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| Submission declined on 17 July 2025 by Utopes (talk). This draft's references do not show that the subject meets Wikipedia's criteria for inclusion. The draft requires multiple published secondary sources that:
Declined by Utopes 8 months ago.
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| This is a copy of an article written using an LLM and is kept for documentation purposes. It is ineligible for speedy deletion under CSD G15 as it has been asserted to be useful to Wikipedia. If you believe it should be deleted, please nominate it on Wikipedia:Miscellany for deletion. |
Comment: Does not seem to have enough significant coverage from independent, reliable sources, per Wikipedia's general notability guidelines. The specifications section is an estimate, and is also entirely unsourced in the article. Utopes (talk / cont) 00:52, 17 July 2025 (UTC)
Goebel Goe II
The Goebel Goe II was a seven-cylinder rotary aircraft engine produced in the German Empire during World War I by Gandenberger’sche Maschinenfabrik Georg Goebel.[1] It was designed in the tradition of French rotary engines such as the Gnome and Le Rhône, which influenced much of Germany’s early aviation propulsion development.
Design and development
The Goebel Goe II was a seven-cylinder, air-cooled rotary engine producing approximately 110 horsepower (82 kW). The entire engine rotated around a stationary crankshaft, a typical feature of rotary engines of the period. It had a diameter of approximately 980 mm and employed a total-loss lubrication system.[1] These characteristics aligned closely with French Gnome-type designs, particularly the Gnome Delta.[2]
Although technically sound, the Goe II was produced only in limited numbers. As the war progressed, German engine development shifted toward more efficient inline and radial engines, which offered improved cooling and better fuel economy.
Operational history
The Goe II powered the Alter A.I, a German single-seat biplane fighter prototype evaluated in early 1917. Although the aircraft reached the flight test stage, it was not selected for further production, and no known surviving examples remain.[3]
In later wartime or postwar service, some Fokker Dr.I triplanes are believed to have been retrofitted with Goebel Goe II engines when converted to training use, though documentation is limited and this remains a secondary reference in some aviation publications.[2]
Applications
Specifications
| Specification | Detail |
|---|---|
| Type | 7-cylinder air-cooled rotary engine |
| Power output | 110 hp (82 kW) |
| Diameter | Approximately 980 mm |
| Configuration | Rotary (engine rotates with propeller around a fixed crankshaft) |
| Lubrication | Total-loss oiling system |
Legacy
The Goebel Goe II is a little-documented but illustrative example of Germany's experimentation with rotary engine technology during World War I. Though it saw only limited application, it contributes to the broader history of early aviation engineering and reflects the influence of French rotary designs on German manufacturers. No surviving examples are known, and its production appears to have ceased by the end of the war.[2]

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