- Design and development
- Specifications (before reconstruction)
- 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 developmentThe 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= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |height m= |height ft= |height in= |height note= |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= |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note=
|perfhide= |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= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |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= |ferry range note= |endurance= |ceiling m= |ceiling ft= |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= |thrust/weight= |more performance=
|guns= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
References }}{{Siemens-Schuckert aircraft}} 5 : Triplanes|German fighter aircraft 1910–1919|Siemens-Schuckert aircraft|Single-engined tractor aircraft|Aircraft first flown in 1917 |