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F r o m W i k i p e d i a , t h e f r e e e n c y c l o p e d i a
( R e d i r e c t e d f r o m G ö p p i n g e n G ö 5 )
The Hütter Hü 17 , is a German high-wing , strut-braced , single-seat, utility training glider that was designed by brothers Ulrich Hütter and Wolfgang Hütter in the 1930s.[1] [2]
The aircraft's correct designation is unclear and various sources refer to is as the Hütter Hü 17, Hütter-17, Hütter H-17, Hutter H-17, Hütter Hü-17, Göppingen Gö 5 and Goppingen 5.[1] [2] [3] [4]
Design and development [ edit ]
The Hütter brothers designed the Hü 17 in Salzburg, Austria , the designation indicating the aircraft's glide ratio . The design was made available as plans for amateur construction and several hundred were completed. The brothers then joined the Schempp-Hirth company which constructed about five of the aircraft under the designation Göppingen Gö 5.[1] [2]
The aircraft is of wooden construction, using a D-tube wing with a single strut and doped aircraft fabric covering . The wing employs a Göppingen 535 airfoil at the wing root and a NACA M-6 at the wing tip . The fuselage is plywood covered.[1] [2] [5]
Operational history [ edit ]
In the 1980s a number of aircraft were still flying in Australia , West Germany , the United Kingdom and the United States .[1] In July 2011 one example was registered with the American Federal Aviation Administration in the Experimental - Exhibition category, having been constructed in 1990.[6]
Variants [ edit ]
Hü 17B in the Technisches Museum Wien
Hü 17
Initial model with a 9.7 m (31.8 ft ) wing span[1] [2]
Hü 17B
Improved model, introduced after the Second World War with increased wing span and higher empty and gross weights[1] [2]
Göppingen Gö 5
Model built by Schempp-Hirth [1] [2]
TG-24
USAAF designation for one impressed Gö 5 (serial number 42-57185 )[7]
CAT 20
Italian licence build, 1938. Over 20 produced.[8]
Aircraft on display [ edit ]
Specifications (Hü 17b) [ edit ]
Data from Sailplane Directory and Soaring [1] [2] and The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde [9]
General characteristics
Crew: one
Length: 5.18 m (17 ft 0 in )
Wingspan: 9.96 m (32 ft 8 in )
Wing area: 9.47 m 2 (101.9 sq ft )
Aspect ratio : 10.5:1
Airfoil : root: Göttingen 535, tip NACA M-6
Empty weight: 110 kg (243 lb )
Max takeoff weight: 210 kg (463 lb )
Performance
Never exceed speed : 160 km/h (99 mph, 86 kn )
Aerotow speed: 100 km/h (62 mph; 54 kn )
Winch launch speed: 80 km/h (50 mph; 43 kn )
Maximum glide ratio: 17:1 at 64 km/h (40 mph)
Rate of sink: 0.98 m/s (192 ft/min) at 61 km/h (38 mph)
Wing loading: 22.2 kg/m2 (4.5 lb/sq ft )
See also [ edit ]
Aircraft of comparable role, configuration, and era
Related lists
References [ edit ]
^ a b c d e f g h Activate Media (2006). "Goppingen 5 Hutter 17" . Archived from the original on 22 March 2012. Retrieved 13 July 2011 .
^ a b National Soaring Museum (2011). "Sailplanes in Our Collection" . Archived from the original on May 16, 2011. Retrieved 31 July 2019 .
^ Federal Aviation Administration (July 2011). "Make / Model Inquiry Results" . Archived from the original on 5 March 2016. Retrieved 31 July 2019 .
^ Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage" . Archived from the original on 20 April 2010. Retrieved 1 July 2011 .
^ Federal Aviation Administration (July 2011). "Make / Model Inquiry Results N17HU" . Archived from the original on 4 March 2016. Retrieved 14 July 2011 .
^ https://usmilitaryaircraft.files.wordpress.com/2015/05/airf-tg.pdf [bare URL PDF ]
^ Pedrielli, Vincenzo; Camastra, Francesco (2011). Italian Vintage Sailplanes . Königswinter: EQIP Werbung & Verlag GmbH. pp. 134–5. ISBN 9783980883894 .
^ Shenstone, B.S.; K.G. Wilkinson; Peter Brooks (1958). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde (in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 9–13.
Shenstone, B.S.; K.G. Wilkinson; Peter Brooks (1958). The World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs dans Le Monde (in English, French, and German) (1st ed.). Zurich: Organisation Scientifique et Technique Internationale du Vol a Voile (OSTIV) and Schweizer Aero-Revue. pp. 9–13.
External links [ edit ]
t
e
Wooden construction
GRP construction
t
e
USAAC/USAAF sequences (1924-1947)
Assault Glider
Bomb Glider
Cargo Glider
Fuel Glider
Powered Glider
Training Glider
1948 USAF redesignations
Tri-service sequence (1962-present)
1 Not assigned
R e t r i e v e d f r o m " https://en.wikipedia.org/w/index.php?title=Hütter_Hü_17&oldid=1191097123 "
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