| SZD-6x Nietoperz | |
|---|---|
.jpg) SZD-6x Nietoperz in thePolish Aviation Museum (SP-1220) | |
| General information | |
| Type | Glider aircraft |
| National origin | Poland |
| Manufacturer | SZD |
| Status | Displayed in museum |
| Number built | 1 |
| History | |
| Introduction date | 1952 |
| First flight | 2 February 1951[1] |
| Retired | 1964 |
TheSZD-6x Nietoperz was a single-seat tail-less experimentalglider aircraft that was designed and built inPoland atSzybowcowy Zakład Doświadczalny (Glider Experimental Works) inBielsko-Biała in 1951.[1] Only one example was constructed (with registration SP-1220).
The SZD-6x Nietoperz (Bat) was designed and built to research tail-less aircraft, and the control of them. Main designers were Władysław Nowakowski and Justyn Sandauer.[1] Built in a conventional fashion using wood throughout, fabric covering and steel for highly stressed parts and fittings the SZD-6x was a cantilever monoplane with the cranked wing attached to a short fuselage pod at the mid position. The inner portion of each wing was markedly swept forward out to approx. quarter-span, where the swept-back outer wing panels were attached.[2] This is arrangement allowed for maximum distance between the centre of gravity and thevertical stabilizer, and placed the pilot at the centre of gravity, so that differing pilot weights had little impact on stability.
The first 'hop' was made on 5 January 1951 atBielsko to test control effectiveness and stability. For more comprehensive trials the glider was transported toKatowice airfield which suffered less turbulence from high ground. On 12 January 1951, the pilotAdam Zientek took an exploratory aero-tow behind aPWS-26 piloted by T. Hill, which nearly ended in disaster. The SZD-6x suffered PIOs (pilot induced oscillations) while still at low altitude over the airfield, hit the ground hard and was damaged.[1] The first "real" flight took place on 2 February 1951, flown by A. Zientek.[1] Later flights were completed successfully, but all the pilots agreed that the aircraft was not suitable for production due to inherent control problems.[1]
The control system of the SZD-6x was designed to allow the aircraft to be flown with several different control configurations. The trailing edges of the wings carried three surfaces each, all of which could be linked to form elevons or operated individually as ailerons, elevators or flaps. The metal-skinned split ailerons, (the outboard control surfaces), also formed theairbrakes, opening out to give increased drag. The ailerons/airbrakes could be connected to the rudder pedals to be used as drag rudders, similar to the drag rudders used on theNorthrop flying wings.[2] The inboard control surfaces on the swept ford section of trailing edge were typically used for trimming purposes deflecting 10° up or down.
The controls were tested in three configurations:
The prototype was used in the SZD for experimental purpose between 18 April 1952 and 26 February 1964, and it also took part in several air shows, even performingaerobatics.[3] With the interesting flying characteristics of the SZD-6x most pilots were not keen to fly the aircraft but Adam Zientek persevered for some time before the aircraft was retired to the Kraków Aviation Museum in 1964.[2]
Data fromThe World's Sailplanes:Die Segelflugzeuge der Welt:Les Planeurs du Monde Volume II[1][4]
General characteristics
Performance
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