Aviatik C.VIII

{{short description|WWI German observation aircraft}}

{{Infobox Aircraft Begin

|name=C.VIII

|image=Aviatik C.VIII-1.jpg

|caption=An oblique view of the Aviatik C.VIII

}}{{Infobox Aircraft Type

|type=Reconnaissance aircraft

|manufacturer=Aviatik

|designer=

|first flight=1917

|number built=1

}}

The Aviatik C.VIII was a prototype German observation aircraft built by Aviatik in World War I.

Design

The C.VIII was a development of the C.VII with the former's BMW IV engine replaced by the simpler Benz Bz.IV. It was an aerodynamically clean biplane with a minimum amount of biplane box struts and a cut-out in the upper wing to improve visibility from the cockpit. Like the Halberstadt CL.II, the Aviatik C.VIII had a plywood-covered fuselage tapering down to a narrow tail.Treadwell, Terry, 2010. German and Austro-Hungarian Aircraft Manufacturers 1908-1918. Stroud: Amberley Publishing.

The Aviatik C.VIII was judged obsolete in 1917 given the deployment of an observer in front of the pilot.

Specifications

{{Aircraft specs

|ref=,{{cite book |last=Gray |first=Peter |last2=Thetford |first2=Owen |title=German Aircraft of the First World War |year=1970 |publisher=Putnam |location=London |isbn=0-370-00103-6 |edition=2nd |page=282}} Aviatik aircraft of WWI : a centennial perspective on great war airplanes{{cite book |last1=Herris |first1=Jack (Author) |last2=Pearson |first2=Bob (Illustrator) |last3=Weaver |first3=Aaron (Cover Design) |title=Aviatik aircraft of WWI : a centennial perspective on great war airplanes |date=14 March 2014 |publisher=Aeronaut Books |isbn=978-1935881223}}

|prime units?=met

|crew=2

|capacity=

|length m=7.3

|span m=10

|width m=

|height m=2.85

|wing area sqm=28

|aspect ratio=

|airfoil=

|empty weight kg=780

|gross weight kg=1180

|max takeoff weight kg=

|fuel capacity=

|more general=

|eng1 number=1

|eng1 name=Benz Bz.IV

|eng1 type=6-cylinder water-cooled in-line piston engine

|eng1 hp=200

|prop blade number=2

|prop name=fixed-pitch propeller

|prop dia m=

|prop dia ft=

|prop dia in=

|prop dia note=

|max speed kmh=170

|max speed mach=

|cruise speed kmh=155

|stall speed kmh=

|never exceed speed kmh=

|minimum control speed kmh=

|range km=

|combat range km=

|ferry range km=

|endurance=

|ceiling m=5100

|g limits=

|roll rate=

|climb rate ms=

|time to altitude=

|wing loading kg/m2=

|fuel consumption kg/km=

|power/mass=

|thrust/weight=

|more performance=

|guns=One flexible {{cvt|7.92|in|3}} Parabellum MG 14 machine gun in the rear cockpit

|bombs={{cvt|60|kg}} of bombs

}}

References

{{Reflist}}

Further reading

  • {{cite book |title=Jane's Encyclopaedia of Aviation |last=Taylor |first=Michael J.H. |year=1989 |publisher=Studio Editions |location=London |isbn=978-0-517-69186-1}}