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词条 Ścibor-Rylski ŚR-3
释义

  1. Design and development

  2. Specifications

  3. References

name=Ścibor-Rylski ŚR-3 image= caption=

}}{{Infobox Aircraft Type

type=Single-seat ultralight national origin=Poland manufacturer= designer=Adam Ścibor-Rylski first flight=Late August 1939 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
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The Ścibor-Rylski ŚR-3 was a Polish, ultralight, low power, single-seat sports aircraft. First flown in August 1939, only one was completed before World War II.

Design and development

Like many amateur Polish designers in the 1930s, Adam Ścibor-Rylski was interested in simple, low cost machines. A student at the Warsaw Technical University, he began his studies with the ŚR-1, an attempt to motorize the Wrona basic, open-frame glider. Difficulties in mounting an engine in this structure led to the ŚR-2 which had the Wrona wing married to a new nacelle. By 1937 he had dropped these projects in favour of a more refined, cabin aircraft. This, the ŚR-3, was the subject of his diploma. With the encouragement of LOPP and the Silesian Gliding Workshop (SWS) he received government funding.

The ŚR-3 was a wooden aircraft with a high cantilever wing. The wing was a one piece structure built around a single spar and tapered in plan. It was plywood covered apart from a small fabric covered area aft of the auxiliary spar that carried the ailerons. These were unbalanced and operated differentially.

It was first fitted with a {{convert|25|hp|kW|disp=flip|abbr=on}} Avia 4 flat-four engine which failed during ground trials and was replaced by a {{convert|30-32|hp|kW|disp=flip|abbr=on}} Sarolea Albatros flat twin with a fuel tank in the wing. Behind the engine the fuselage was a rectangular section, stressed ply skinned structure, with a rounded roof between the wing trailing edge and the tail where the fuselage narrowed strongly in profile. The ŚR-3's single-seat cockpit was under the wing leading edge and had an upward hinged, one-piece transparent cover.

Its empennage was also ply covered and unbalanced, with the tailplane mounted on top of the fuselage. The fin was almost triangular and carried a full, semi-elliptical rudder which operated between the elevators.

The ŚR-3 had small mainwheels mounted close to the fuselage on short, curved V-struts which had a rubber-in-compression shock absorber within the fuselage.

Zbiniew Żabski flew the ŚR-3 on its first flight at the end of August 1939. Though SWS had hoped to produce the ŚR-3 in both kit and complete forms, the German invasion of Poland a few days after the first flight ended such hopes. The ŚR-3 was reportedly taken by the invaders and flown by the Dortmund Nazi youth organisation.

Specifications

{{Aircraft specs
|ref=J. Cynk (1971) (Dimensions approximate)
|prime units?=met


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|crew=One
|length m=6.5
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|span m=8
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|empty weight kg=160
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|gross weight kg=250
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|more general=


|eng1 number=1
|eng1 name=Sarolea Albatros
|eng1 type=air-cooled flat twin
|eng1 hp=30-32
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|perfhide=
|max speed kmh=
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|cruise speed kmh=
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|stall speed kmh=
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|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=
|range miles=
|range nmi=
|range note=
|endurance=2 h
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
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|wing loading kg/m2=
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}}

References


}}

1 : Polish sport aircraft 1930–1939

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