Schleicher Ka 6

External image
External image
	<img alt="image icon" src="//upload.wikimedia.org/wikipedia/en/thumb/6/61/Searchtool.svg/16px-Searchtool.svg.png" decoding="async" width="16" height="16" class="mw-file-element" data-file-width="512" data-file-height="512"> Ka 6E with open cockpit

Ka 6
Ka 6
	Ka 6 on display in the Deutsches Museum, Munich
General information
Type	Club class glider
Manufacturer	Alexander Schleicher GmbH & Co
Designer	Rudolf Kaiser
Number built	> 1000 (all variants)
History
First flight	1955

The Schleicher Ka 6 is a single-seat glider designed by Rudolf Kaiser,^[1] built by Alexander Schleicher GmbH & Co, Germany and is constructed of spruce and plywood with fabric covering. The design initially featured a conventional tailplane and elevator which was later replaced by an all-moving tailplane in the -Pe and Ka 6E variants. Variants built before the -CR and -BR used a main skid as the principal undercarriage, with later variants including the Ka 6E using a wheel as the main undercarriage with no nose skid. Other modifications for the Ka 6E include a more aerodynamic fuselage with glassfibre nose and wingroot fairings, longer canopy, and modified aluminium airbrakes.

Variants

KA 6E G-DCCV at the Vintage Glider Rally at Camphill, 2011

Mr. and Mrs. Fritz Sebek preen their Ka-6BR at Harris Hill, New York.

Dates of initial airworthiness approval in brackets:

Ka 6 – Initial version; span 14.4 m (47 ft 3 in), (30 October 1956).
Ka 6B (27 September 1957).
Ka 6B-Pe – The Ka 6B with all-flying tailplane, (20 May 1960).
Ka 6BR – The Ka 6B with the main skid removed and a relocated mainwheel, (27 September 1957).
Ka 6CR – The Ka 6C with the main skid removed and a relocated mainwheel, (24 February 1959).
Ka 6CR-Pe – The Ka 6CR with all-flying tailplane, (20 May 1960).
Ka 6E The ultimate Ka-6, with all-flying tailplane, (29 July 1965).

Aircraft on display

US Southwest Soaring Museum – Ka 6B-Pe and Ka 6e^[2]

Specifications (Ka 6E)

Data from ^[3]

General characteristics

Crew: 1
Length: 6.66 m (21 ft 10.25 in)
Wingspan: 15 m (49 ft 2.5 in)
Height: 1.6 m (5 ft 3 in)
Wing area: 12.4 m² (135.5 sq ft)
Aspect ratio: 18.1
Airfoil: Root: NACA 633-618 Mid: NACA 633-614 (with Wortmann leading edge modification)
Empty weight: 190 kg (419 lb)
Gross weight: 300 kg (661 lb)

Performance

Maximum speed: 200 km/h (124 mph, 108 kn)
Maximum glide ratio: 32:1 at 80 km/h (50 mph)
Rate of sink: 0.65 m/s (128 ft/min)

References

Notes

^ Segelflugzeugbau, Alexander Schleicher | (2016-04-26). "K 6 E | ASSegelflug" (in German). Retrieved 2023-09-03.
^ US Southwest Soaring Museum (2010). "Sailplanes, Hang Gliders & Motor Gliders". Retrieved 26 May 2011.
^ Coates, 1978. p. 86.

Bibliography

Coates, Andrew, Janes World Sailplanes and Motorgliders. London. Macdonald and Jane's Publishers Ltd., 1978. ISBN 0-354-01119-7

Macfadyen, Tim. BGA Data sheet for Schleicher Ka-6, BR and CR (Rhönsegler). Leicester. British Gliding Association. 1 July 2003.

External links

[1] Segelflugzeugbau, Alexander Schleicher | (2016-04-26). "K 6 E | ASSegelflug" (in German). Retrieved 2023-09-03.

[SWSMCollection-2] US Southwest Soaring Museum (2010). "Sailplanes, Hang Gliders & Motor Gliders". Retrieved 26 May 2011.

[3] Coates, 1978. p. 86.

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