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New open class glider

Be 23

Well-known member
Joined
Feb 10, 2006
Posts
127
Total Time
3500
Type description
Body:
Shell fuselage from fiber composite material (CFRP and aramid)
comfortable spacious cockpit for large pilots
opening after front top hood with a sliding Windows and Lüftungsklappe
Instrument panel swing with the hood upwards
TOST security coupling (for aircraft towing)
Total pressure to the fuselage tip.
Capture to TEK nozzle in the page fin static print picking (for trip meters and altimeter) on both sides of the rear fuselage tube cockpit:
removable Schalensitz
Anschnallgurt with quick closure
Seat cushion
Ventilation by admission to the fuselage nose with anti fitting cooling the hood
adjustable ventilation right side
Control:
adjustable in flight page pedals
Control rods from carbon fiber
Trim electrically adjustable with control button on the stick
Automatic Höhenruder port
Suspension and brake:
Chassis electrically einzieh and extendable
Spring suspension
hydraulic disc brake
Spur wheel
Engine:
Engine einklappbar in the short tube
Solo motor 2625 / 2
long toothed belts with gearbox 1: 3 and centrifugal force-slip coupling integrated in the dental Riemenantrieb for the propeller for better quietness of the engine and longer life of timing belt
Water cooling
Double ignition
electric starter
LiMg batteries with 16,8V load final voltage for improved inputs and lead out and starting the engine
Engine monitoring instrument in the instrument panel
Propeller Binder BM-G1-160-R-120-1 in fiber Verbundbauweise
Fuel tank:
in the body ~ 22 litres
Integral fuel tank in the inner wing with ~ 11 ltr capacity per wing
Antenna:
Antennae in the rudder
Wings:
8-teiliger wing with Wing influence at the bottom of the wing wing tail with winglet for 28.3 bezw. 29.3 m span interchangeable
constructed of high engine fiber using
Slot cover on the rowing with Maylarband
Doppelstöckige braking flaps at the wing top
Water ballast:
Water ballast bags in the external wings each with ~ 50 litres capacity
Water ballast bags in the inner wings each with ~ 60 litres capacity
Water ballast tail tank in the Seitenleitwerk for settlement of gravity when water ballast in the wing
Finish and design:
Two components white polyester coating or PU coating
The main components such as fuselage and wing and various other components in the vacuum process are built to optimize weight. This allows a wide margin for the surface load.
EASA type certification out estimated in the autumn 2010.
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Bank-n-Yank

Active member
Joined
Dec 25, 2002
Posts
41
Total Time
<6000
What are the claimed L/Dmax & min sink figures?
 
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