Siemens-Schuckert R.VIII

{| Đế quốc Đức
| manufacturer= Siemens-Schuckert (Siemens-Schuckert Werke G.m.b.H., Siemensstadt. Berlin)
| designer=
| first flight=
| introduced=
| retired=
| status=
| primary user=
| number built= 2 (1 chưa hoàn thành)
|prime units?=met

|genhide=

|crew=6+
|capacity=
|length m=21,6
|length ft=
|length in=
|length note=
|span m=48
|span ft=
|span in=
|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=
|swept m=
|swept ft=
|swept in=
|swept note=
|dia m=
|dia ft=
|dia in=
|dia note=
|width m=
|width ft=
|width in=
|width note=
|height m=7,4
|height ft=
|height in=
|height note=
|wing area sqm=440
|wing area sqft=
|wing area note=
|swept area sqm=
|swept area sqft=
|swept area note=
|volume m3=
|volume ft3=
|volume note=
|aspect ratio=
|airfoil=
|empty weight kg=
|empty weight lb=23.100
|empty weight note=
|gross weight kg=
|gross weight lb=34.980
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|lift kg=
|lift lb=
|lift note=
|more general=

|eng1 number=6
|eng1 name=Basse & Selve BuS.IVa
|eng1 type=kiểu động cơ piston thằng hàng 6 xy-lanh, làm mát bằng nước
|eng1 kw=
|eng1 hp=300
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|eng1 kn-ab=
|eng1 lbf-ab=

|eng2 number=
|eng2 name=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 note=
|eng2 kn-ab=
|eng2 lbf-ab=

|eng3 number=
|eng3 name=
|eng3 type=
|eng3 kw=
|eng3 hp=
|eng3 kn=
|eng3 lbf=
|eng3 note=
|eng3 kn-ab=
|eng3 lbf-ab=
|more power=

|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=

|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=

|perfhide=

|max speed kmh=125
|max speed mph=
|max speed kts=
|max speed note=
|max speed mach=
|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=900
|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=4.000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|sink rate ms=
|sink rate ftmin=
|sink rate note=
|lift to drag=
|wing loading kg/m2=35
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=

|power/mass=
|thrust/weight=

|more performance=
Giá thành – 750.000 Mark

|armament=
|guns=
|bombs=
|rockets=
|missiles=

|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=

|other armament=

|avionics=
}}

Xem thêm

Tham khảo

Haddow, G.W. & Grosz, Peter M. The German Giants, The Story of the R-planes 1914-1919. London. Putnam. 1963.
Gray, Peter & Thetford, Owen. "German Aircraft of the First World War". London, Putnam. ISBN 0-370-00103-6
Sollinger, Guenther, "Villehad Forssman: Constructing German Bombers 1914-1918. Moscow, Rusavia, 2009.