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词条 Siemens-Schuckert Dr.I
释义

  1. Design and development

  2. Specifications (before reconstruction)

  3. References

name=Dr.I image= caption=

}}{{Infobox Aircraft Type

type=Triplane fighter aircraft national origin=Germany manufacturer=Siemens-Schuckert designer= first flight=July 1917 introduced= retired= status= primary user= more users= produced= number built=1 program cost= unit cost= developed from= variants with their own articles=
}}

The Siemens-Schuckert Dr.I was a German single seat triplane fighter aircraft first flown in 1917. Its development and that of a more powerful, uncompleted variant, was abandoned after a flight test programme.

Design and development

The Dr.I was a single seat triplane developed at the same time as the Siemens-Schuckert D.II. It used the flat sided fuselage of the earlier Siemens-Schuckert D.I biplane rather than that of the rounded D.II. Like the D.I the Dr.III was powered by a {{convert|110|hp|kW|abbr=on|0}} Siemens-Halske Sh.I nine cylinder rotary engine.

The fighter was first flown in July 1917. Later in its development programme the Dr.I crashed and was seriously damaged. Siemens-Schuckert rebuilt it, though adding 2.90 m2 (31.2 sq ft) to the wing area.

Construction of a version powered by a more powerful {{convert|110|hp|kW|abbr=on|0}} Siemens-Halske Sh.III eleven cylinder rotary engine, the Dr.II, was well advanced when it was abandoned.

Specifications (before reconstruction)

{{Aircraft specs
|ref=The Complete Book of Fighters p.529
|prime units?=met


|genhide=
|crew=One
|length m=5.30
|length note=
|span m=8.60
|span note=
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|mid span m=
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|height m=
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|wing area sqm=18.10
|wing area note=
|aspect ratio=
|airfoil=
|empty weight kg=510
|empty weight note=
|gross weight kg=695
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Siemens-Halske Sh.I
|eng1 type=9-cylinder rotary
|eng1 hp=110
|eng1 note=
|power original=
|more power=
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|perfhide=
|max speed kmh=
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|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=
|minimum control speed kmh=
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|minimum control speed note=
|range km=
|range miles=
|range nmi=
|range note=
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
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|endurance=
|ceiling m=
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|ceiling note=
|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=20.6 min to 4,700 m (15,420 ft) post-rebuild
|lift to drag=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|power/mass=
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|guns=
}}{{aircontent
|see also=
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|lists=
}}

References


}}{{Siemens-Schuckert aircraft}}

5 : Triplanes|German fighter aircraft 1910–1919|Siemens-Schuckert aircraft|Single-engined tractor aircraft|Aircraft first flown in 1917

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