Oct 17, 2012, 05:38 AM
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Joined Sep 2011
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K 8
Role Sailplane
National origin Germany
Manufacturer Schleicher
Designer Rudolf Kaiser
First flight November 1957
Number built over 1,100
K8 in red/yellow livery (EUGC)
The Schleicher K 8 is a single-seat glider designed by Rudolf Kaiser and built by the Alexander Schleicher company of Germany.
[edit]Design and development
The K 8 was derived from the earlier Ka 6 design as a simple single-place sailplane with dive brakes using construction techniques similar to the Schleicher K 7, simplified for amateur construction from kits. Emphasis was on rugged construction, good climbing ability in thermals and good handling characteristics.
The prototype K 8 made its first flight in November 1957 and over 1,100 were built in three main versions. The original K 8 had a very small canopy. Side windows for improved visibility were introduced in the next version, and the K 8B, by far the most numerous variant, has a larger one-piece blown Plexiglas canopy. The K 8C features a longer nose, larger main wheel located ahead of the center of gravity and deletion of the larger wooden nose skid resulting in a roomier cockpit.
The cantilever high wings are single-spar structures of pine and plywood, with a plywood leading edge torsion box and fabric covering aft of the spar; the forward sweep is 1° 18' and dihedral is 3°. There are Schempp-Hirth air brakes in the upper and lower surfaces and the wooden ailerons are plywood covered. The cantilever tail unit is of similar construction to the wings, with ply-covered fixed surfaces and fabric-covered rudder and elevators, and a trim tab in the elevator is an optional fitting. The fuselage is a welded steel-tube structure, with fabric covering over spruce longerons and a glass fibre nose cone.
There is a non-retractable and unsprung monowheel, with optional brake, and a nose skid mounted on rubber blocks in front of it, plus a steel skid at the tail.
[edit]Operational history
Karl Striedieck of the United States made a 767 km / 476.6 mile ridge flight in a K 8B to establish a world out-and-return record in 1968.
[edit]Motor glider variants
A motor glider conversion of the K 8B was developed by LVD (the Flying Training School of the Detmold Aero Club) similar to their conversion of a Scheibe Bergfalke IV known as the BF IV-BIMO, in which a Lloyd LS-400 piston engine mounted in the fuselage drives a pair of small two-blade pusher propellers rotating within cutouts in each wing near the trailing edge.
Another motorglider conversion was used by "Vestjysk Svæveflyveklub" in Denmark: it had a small Wankel rotary engine mounted in a nacelle on an aluminium stick above the main spar. The engine wase started with a recoil starter like a lawn mower. The high RPM of the device made it extremely unpopular: the propeller tips created a permanent sonic boom, that made the plane extremely noisy. The harassed citizens of Esbjerg nicknamed the plane 'the flying circular saw' and the engine was removed.[citation needed]
[edit]Specifications ( K 8B)
K 8b
K 8 b G-CJOB landing at Camphill
Data from Jane's All The World's Aircraft 1966–67[1]
General characteristics
Crew: One
Length: 7.00 m (23 ft 0 in)
Wingspan: 15.00 m (49 ft 2½ in)
Height: 1.57 m (5 ft 1¾ in)
Wing area: 14.15 m2 (152.3 ft2)
Aspect ratio: 15.9:1
Wing profile: Göttingen 533/532
Empty weight: 195 kg (430 lb)
Gross weight: 310 kg (683 lb) each each
Performance
Maximum speed: 190 km/h (118 mph)
Maximum glide ratio: 27:1
Rate of sink: 0.72 m/s (142 ft/min)
[edit]References
^ Taylor 1966, pp. 393–394.
Taylor, John W. R. Jane's All The World's Aircraft 1966–67. London:Sampson Low, Marston & Company, 1966.
Schleicher Web Site
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