请输入您要查询的百科知识:

 

词条 Siegel MS 2
释义

  1. Design and development

  2. Operational history

  3. Variants

  4. Specifications (MS 2)

  5. References

name=Siegel MS 2 image= caption=

}}{{Infobox aircraft type

type= Glider national origin=Poland manufacturer= designer=Mieczysław Siegel first flight=1924 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Siegel MS 2 was a Polish, amateur-built glider incorporating lessons learned from his first design. It first flew in 1924 but had only a brief career. In 1925 an improved variant, the MS 3, flew briefly.

Design and development

Mieczysław Siegel, a schoolteacher from Skrynice near Lublin, designed and built his first aircraft, the Speigel MS 1, in the school summer holidays of 1923. It was a simple, small and very light foot-launched glider. Over the next summer he built its improved successor, the MS 2. This retained the earlier glider's low cost paper and card covering over a simple wooden structure but was no longer foot launched, allowing a conventional cockpit. It also had a simpler wing and a more conventional, less vulnerable tail.[2]

Like its predecessor, the MS 2 had its high wing on top of the fuselage. The rectangular plan wing was built around two spars, covered with wrapping paper stiffened with gelatin. The forward spar was braced with a strut to the lower fuselage and the rear one by wire, allowing lateral control by wing warping as used on the MS 1.

The cardboard covered fuselage had a rectangular section which tapered rearwards more strongly than that of the MS 1 and had an open cockpit overlooking the mid-wing. The MS 2's tail surfaces were all paper-covered, with a tailplane that was triangular as before but less broad in chord and mounted at mid-fuselage. It carried a one-piece, large area elevator. The fin was now conventionally on top of the fuselage, triangular in profile and with a rhomboidal rudder which gave the elevator clearance to move upwards.[2]

The MS 3 was a final development. It was broadly similar to the MS 2 but the wing strut was replaced by wire and the paper and card covering by fabric. There was no fin and it had new, cross-axle, wheeled landing gear.[6]

Operational history

Both the MS 2 and MS 3 had short lives. At the first attempts to rope-launch the former, the wind dropped and it would not take-off with a pilot aboard. To please the crowd Siegel flew it empty, as a kite. It performed well several times, then destabilized and crashed to destruction.

The MS 3's new landing gear proved a handicap, tending to sink into soft ground and making rope launches more difficult. Short hops were made with rope launches though it is not known if the rope was cleared. After its flying life ended in a crash it was repaired, then exhibited at an aeronautics show at Lublin.[6]

Variants

MS 2
1924 revision of MS 1. Slightly larger all round, new wing with rigid forward braces; new empennage. Rope launched so conventional cockpit.
MS 3
1925 revision of MS 2. Few details available, but with new undercarriage and fabric covered, all-wire wing bracing and finless.

Specifications (MS 2)

{{Aircraft specs
|ref=Samolotypolskie.pl[2]
|prime units?=met


|genhide=
|crew=One
|capacity=
|length m=4.5
|length note=
|span m=7
|span note=
|height m=0.85
|height note=[2]
|wing area sqm=8.2
|wing area note=
|aspect ratio=5
|airfoil=
|empty weight kg=35
|empty weight lb=
|empty weight note=
|gross weight kg=110
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|more general=


|perfhide=Y
|max speed kmh=
|max speed mph=
|max speed kts=
|max speed note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|ceiling m=
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=
|wing loading lb/sqft=
|wing loading note=
|power/mass=
|thrust/weight=
|more performance=
}}

References

1. ^{{cite web |url=http://www.samolotypolskie.pl/samoloty/2674/82/MS-22|title=MS-2, 1924|publisher=Samolotypolskie.pl|accessdate=13 January 2019}}
2. ^{{cite web |url=http://www.samolotypolskie.pl/samoloty/2675/126/MS-3|title=MS-3, 1925|publisher=Samolotypolskie.pl|accessdate=17 January 2019}}
[1][2]
}}

1 : Polish sailplanes 1920–1929

随便看

 

开放百科全书收录14589846条英语、德语、日语等多语种百科知识,基本涵盖了大多数领域的百科知识,是一部内容自由、开放的电子版国际百科全书。

 

Copyright © 2023 OENC.NET All Rights Reserved
京ICP备2021023879号 更新时间:2024/11/11 18:54:16