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Göppingen Gö 9

From Wikipedia, the free encyclopedia
German research aircraft
Gö 9
Göppingen Gö-9 motor glider, flying c.1941
General information
TypeExperimental aircraft
National originNazi Germany
ManufacturerSchempp-Hirth
Designer
Ulrich Hütter
Number built1
History
First flight1941, by Dornier Test Pilot Henry H. W. Quenzler
Developed fromDornier Do 17

TheGöppingen Gö 9 was a German experimental aircraft built to investigate the practicalities of powering a plane using apusherpropeller located far from the engine and turned by a long driveshaft.

Design and development

[edit]
Dornier Test Pilot Henry H. W. Quenzler in cockpit of Gö 9 experimental aircraft

In 1937,Claudius Dornier observed that adding extra engines and propellers to an aircraft in an attempt to increase speed would also attract a penalty of greaterdrag, especially when placing two or more engines withinnacelles mounted on the wings. He reasoned that this penalty could be minimized by mounting a second propeller at the rear of an aircraft. To prevent tail-heaviness, however, the engine would need to be mounted far ahead of it. Dornierpatented this idea and commissioned a test plane to evaluate it.

The aircraft was designed by DrUlrich Hütter as a 40% sized, scaled-down version of theDornier Do 17's fuselage and wing panels without the twin-engine nacelles, and built bySchempp-Hirth. The airframe was entirely of wood and used a retractabletricycle landing gear – one of the earliest non-Heinkel-built German airframe designs to use such an arrangement. Power was supplied by aHirth HM 60 inverted, air-cooled inline four-cylinder engine mounted within the fuselage near the wings. Other than the engine installation, the only other unusual feature of the aircraft was its all-new, full four-surfacecruciform tail, which included a large ventral fin/rudder unit of equal area to the dorsal surface. This fin incorporated a small supplementary tailwheel protruding from the ventral fin's lower tip that assisted in keeping the rear-mounted, four-blade propeller away fromtailstrike damage against the ground during take-off and landing. The Gö 9 carried the civil registrationD-EBYW.

Operational history

[edit]

Initially towed aloft, flight tests began in June 1941, but later flights operated under its own power. The design validated Dornier's ideas, and he went ahead with his original plan to build a high-performance aircraft with propellers at the front and rear, producing theDornier Do 335. The test pilot was Henry H. W. Quenzler. The eventual fate of the Gö 9 is not known.

Specifications (Gö 9)

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Data from Die Deutsche Luftruestung 1933-1945 Vol.1 - AEG-Dornier[1]

General characteristics

  • Crew: 1
  • Length: 6.80 m (22 ft 4 in)
  • Wingspan: 7.20 m (23 ft 7 in)
  • Gross weight: 720 kg (1,587 lb)
  • Powerplant: 1 ×Hirth HM 60 4-cyl. inverted air-cooled in-line piston engine, 60 kW (80 hp)
  • Propellers: 4-bladed pusher propeller turned via an extension shaft

Performance

  • Maximum speed: 220 km/h (140 mph, 120 kn)

See also

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Aircraft of comparable role, configuration, and era

Related lists

References

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Citations

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  1. ^Nowarra, Heinz J. (1993).Die Deutsche Luftruestung 1933-1945 Vol.1 - AEG-Dornier. Koblenz: Bernard & Graefe Verlag.ISBN 3-7637-5464-4.

Bibliography

[edit]
  • Nowarra, Heinz J. (1993).Die Deutsche Luftruestung 1933-1945 Vol.1 - AEG-Dornier. Koblenz: Bernard & Graefe Verlag.ISBN 3-7637-5464-4.
  • Selinger, P E.Segelflugzeuge Vom Wolf zum Discus. Motor Buch Verlag, Stuttgart 1989

External links

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Wikimedia Commons has media related toGöppingen Gö-9.
Wooden construction
GRP construction
1 to 100
101 to 200
201 to 300
301 to 349
Post-349 (non-sequential)
  • 1 Not assigned
  • 2 Unofficial/proposed
  • 3 Assigned, but not used before RLM was dissolved
  • 4 Assigned to captured aircraft
  • 5 Unconfirmed
  • 6 Propaganda/cover designation
  • 7 Assigned to multiple types

Note: Official RLM designations had the prefix "8-", but this was usually dropped and replaced with the manufacturer's prefix.

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