- Design and development
- Specifications
- See also
- References
name=C.XIII | image=Albatros C.XIII.jpg | caption= }}{{Infobox Aircraft Type | type=2 seat fighter 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.XIII was a German two-seat, single-engine, biplane light fighter aircraft built in 1917. Only one was constructed. Design and developmentThe C.XIII was built along the lines of the single seat Albatros D.Va but was a two-seater, larger by about 10% in span and by 6% in length. It was intended to fall into the newer Idflieg two seat CL-class, reserved for lighter two-seat fighters. The round cross section, plywood-covered fuselage was, apart from the second, tandem open cockpit similar in appearance to that of the D.Va, smoothly tapering to the nose with lines that merged into those of the spinner. As with the single-seater, the inline Mercedes D.III engine was largely enclosed but had its six upper cylinders exposed. The C.XIII was fitted with an early {{convert|160|hp|kW|abbr=on|0}} unit, less powerful than the D.Va's. The empennage was noticeably different, with a narrower, taller vertical tail. Its straight, constant-chord wings had single bays and were mounted without stagger. The undercarriage was of the fixed type, with mainwheels on V-struts and a faired-in tailskid. First flown in 1917, only one C.XIII was built and the type did not enter production; instead Albatros built the flat-sided, two-bay, more powerful C.XIV the following year for the light two-seat category, developing it into the production C.XV. Specifications{{Aircraft specs |ref=German Aircraft of World War I. |prime units?=met |genhide= |crew=Two |capacity= |length m=7.8 |length note= |span m=10.0 |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |lower span m= |lower span ft= |lower span in= |lower span note= |height m=2.71 |height note= |wing area sqm= |wing area sqft= |wing area note= |aspect ratio= |airfoil= |empty weight kg=700 |empty weight note= |gross weight kg=1060 |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 |eng1 note= |power original= |more power= |prop blade number=2 |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop dia note=
|perfhide= |max speed kmh=165 |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=2.5 hr |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude=47 min to 5,000 m (16,400 ft) |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |power/mass= |more performance=
|guns=1×Spandau machine gun and 1×Parabellum MG14 machine gun |bombs= }}
See also{{aircontent |see also= |related= |similar aircraft= |lists= }}References{{Commons category}} }}{{Albatros aircraft}} 2 : Albatros aircraft|German fighter aircraft 1910–1919 |