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词条 Jancsó-Szokolay M22
释义

  1. Design and development

  2. Operational history

  3. Specifications

  4. References

name=Jancsó-Szokolay M22 image= caption=

}}{{Infobox aircraft type

type=High performance sailplane national origin=Poland manufacturer=MrSE workshop and elsewhere designer=Endre Jancsó and András Szokolay first flight=1 September 1937 introduced= retired=1952-3 status= primary user= more users= produced= number built=20 program cost= unit cost= developed from= variants with their own articles=
}}

The Jancsó-Szokolay M22 was a Hungarian single-seat sailplane first flown in 1937. Twenty were built and the type set several national records. Some remained in service up to about 1953.

Design and development

In the mid-1930s the MSrE (Műegyetemi Sportrepülő Egyesület) or Aero Club of the Technical University decided to build a sailplane capable of thermal, cross country fights. They began to build a Rhönbussard but Erno Rubik encouraged Endre Jancsó and András Szokolay to design a new, Hungarian aircraft incorporating the Rhönbussard parts already completed. The result was the M22 which flew for the first time on 1 September 1937.

The two-part gull wing of the M22 was mounted at mid-fuselage. The central panels were rectangular in plan, occupied about 35% of the span and had 8° of dihedral. The outer panels were trapezoidal apart from rounded tips and had no dihedral. Both panels shared a single spar which, with plywood skinning forward of it around the leading edge, formed a torsion-resistant D-box. The half-wings were joined together within the fuselage. Near the fuselage the plywood extended rearwards to an angled drag strut. The rest of the wing surface was fabric covered. Parallel chord ailerons, mounted on a light false spar, filled the whole trailing edges of the tapered outer parts and could be lowered together as camber-changing flaps. Early examples of the M22 had no air brakes but later Göppingen type brakes, mounted on the rear of the main spar at the start of the drag strut, deployed above and below the wing.[1]

The sailplane had an roughly oval section, ply-covered fuselage, though the sides met at a sharp, linear keel. A rubber-sprung landing skid covered the join from nose to under mid-chord. Its cockpit was at the leading edge and usually enclosed with a canopy modified over the years by the M22's various manufacturers. The fuselage tapered rearwards; the tailplane and elevators together, mounted on top of the fuselage, were straight-tapered out to tapered tips and fabric-covered apart from ply-skinned leading edges. A small, short, ply-covered fin served as a rudder post for the balanced rudder, which was large, curving and with a slightly pointed tip. It was usually fabric-covered, though some manufactured by Aero Ever Ltd. in 1943 were ply-covered.[1]

The M22 was fully aerobatic.[1]

Operational history

Three M22s were built by MSrE, ten more by Aero Ever Ltd and another four by the Aircraft Factory of Transylvania. Three more were built at other aeroclubs.[1]

The first example was bought by the Aero Club of Egypt.[1] In 1938 visiting RAF Squadron Leader Edward Mole was impressed by its qualities and, after a tow by an Avro Tutor, performed a double bunt or outside loop in it.[8]

The M22 set several Hungarian glider records. These included a distance record of {{cvt|356|km| mi nmi}} in 1942 and the greatest height gain {{cvt|3845|m|ft}} in the same year. In 1949 an M22 set a national record of for speed around a {{cvt|100|km|mi nmi}} triangular course of {{cvt|33.4|km/h|mph kn}}.

The remaining M22s were retired in 1952-3.

Specifications

{{Aircraft specs
|ref=M-22, Hungarian gliders 1933-2000, F Gabor[1]
|prime units?=met


|genhide=
|crew=One
|capacity=
|length m=5.8
|length note=
|span m=15
|span note=
|height m=
|height note=
|wing area sqm=16.55
|wing area note=
|aspect ratio=13.55
|airfoil=Göttingen Gö 535 out to NACA 99 tip
|empty weight kg=180
|empty weight note=
|gross weight kg=265
|gross weight note=
|max takeoff weight kg=
|max takeoff weight note=
|more general=


|perfhide=
|max speed kmh=260
|max speed note=VNE
|cruise speed kmh=
||cruise speed note=
|stall speed kmh=55
|stall speed note=
|g limits=
|roll rate=
|glide ratio= best 22 at {{cvt|67|km/h|mph kn}}
|sink rate ms=0.8
|sink rate note=minimum, at {{cvt|60|km/h|mph kn}}
|lift to drag=
|wing loading kg/m2=
|wing loading note=
|more performance=

  • Maximum aerotow speed: {{cvt|120|km/h|mph kn}}

}}

References

1. ^{{cite journal |last=Mole |first=E.L. |date=March 1938 |title=Aerobatics in Egypt|journal= The Sailplane|pages=55 }}
2. ^{{cite web |url=http://gliders-fega.freeweb.hu/szittya-i.html|title=M22, Hungarian gliders 1933-2000 |author=Fekes Gabor |date= |work= |publisher= |accessdate=15 February 2019}}
[1][2]
}}

2 : Aircraft first flown in 1937|Hungarian sailplanes 1930–1939

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