Kestrel 19M Glasflugel   


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General Details
Manufacturer: Glasflugel
Plane Name:

Kestrel 19M

Classified as: Unclassified
Country Of Origin: Germany
Designer: Hanle/Prasser
No. of Seats 1
No. Built 129
   
Performance:
L/DMax: 44 97 kph / 52 kt / 60 mph
   
MinSink: 0.52 m/s / 1.71 fps/ 1.01 kt
   


 

Specifications:
Span Area Empty Weight Payload Gross Weight Wing Load Water Ballast
m ft sq.m sq.ft kg lb. kg lb. kg lb. kg
/sq.m
lb.
/sq.ft
kg lb.
19 62.3 12.87 138.5 330 728 140 309 472 1041 36.65 7.51 0 0
Aspect ratio: 28
Airfoil:
Structure: fiberglass
Engine:

Comment:
The 17 m. Kestrel features camber-changing flaps that operate in conjunction with the ailerons, airbrakes, drogue chute, water ballast and retractable gear. The fuselage is a fiberglass monocoque (not sandwich) for greater resilience and pilot protection. The cockpit has room enough for a 198 cm / 6 ft pilot and features a control stick that slides fore and aft (rather than rotating) to reduce likelihood of pilot- induced oscillations and which has a press-to- trim-push-button trimmer. It has a nose and a center of gravity release. Goran Ax won the second Smirnoff Transcontinental Sailplane Race in a Kestrel in 1973. Sue Martin of Australia gained both the womens world 100 km speed record ( 113.2 kph / 70.36 mph ) and 300 km triangle speed record (114.4 kph/ 71.11 mph). As well as building the 17 m. model under license, Slingsby of Great Britain developed a 19 m. version which first flew in 1971 incorporating a drag reducing wing root fillet and an anti-balance tab on the elevator.


           

Your Comments:
Kestrel Newsgroup - 133 - Posted by: Kestrel254 - george.e@dial.pipex.com (29/Mar/2002) Reply

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