- Design and development
- Specifications
- References
name=C.VIII N | image= | caption= }}{{Infobox Aircraft Type | type=Night bomber aircraft | national origin=Germany | manufacturer=Albatros Flugzeugwerke | designer= | first flight=1917 | introduced= | retired= | status= | primary user= | more users= | produced= | number built=1 | program cost= | unit cost= | developed from= | variants with their own articles= }} |
The Albatros C.VIII N was a German large, single engine biplane bomber, intended for night time operations, It was seriously underpowered and could only carry a small bomb load. Design and developmentThe C.III N was a large but underpowered three bay night bomber, as denoted by the N, its engine only just powerful enough to meet the Idflieg two seat C-class minimum requirement. It had straight edged, constant chord wings of about equal span and with parallel pairs of interplane struts. There were ailerons on both upper and lower planes. A {{convert|160|hp|kW|abbr=on|0|disp=flip}} inline Mercedes D.III mounted in the nose with its upper cylinders exposed drove a two blade propeller, with two tandem, open cockpits aft. The externally braced tailplane was at mid-fuselage height; the fin, broad and almost quadrant-edged, carried a balanced rudder which ended above the elevators. The C.VIII N landed on a fixed conventional undercarriage with a pair of mainwheels on a rigid axle and a tailskid. The C.VIII N first flew in 1917 and it seems likely only one was built. Specifications{{Aircraft specs |ref=German aircraft of the first World War p.257 |prime units?=met |genhide= |crew=2 |capacity= |length m=7.34 |length note= |span m=16.34 |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft= |wing area note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general=
|eng1 number=1 |eng1 name=Mercedes D.III |eng1 type=6-cylinder water cooled inline |eng1 hp=160 |more power= |prop blade number=2 |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note=
|perfhide= |max speed kmh=135 |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= |endurance= |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude=5 min to 1,000 m (3,280 ft) |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |power/mass= |thrust/weight= |more performance=
|guns= 1×Spandau machine gun and 1×Parabellum machine gun |bombs=light load under wing }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
References }}{{Albatros aircraft}} 2 : Albatros aircraft|German bomber aircraft 1910–1919 |