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About: dbkwik:resource/B6SoA5_U649I37SK9X59vA==

PropertyValue
rdf:type
rdfs:label
  • AEG C.VIII
rdfs:comment
  • The AEG C.VIII was a prototype two-seat reconnaissance aircraft of World War I. Two examples were built, based on the successful C.IV design, one of biplane configuration, the other a triplane (the latter sometimes referred to as the C.VIII.Dr). Neither version offered enough of an improvement on the C.IV to make mass production worthwhile.
owl:sameAs
dcterms:subject
dbkwik:military/property/wikiPageUsesTemplate
loaded weight main
  • 1160.0
climb rate main
  • 4.386000
number of props
  • 1
length alt
  • 22
span main
  • 9.5 m
power/mass alt
  • 0.063000
primary user
  • Luftstreitkräfte
Type
type of prop
  • six-cylinder water-cooled inline engine
length main
  • 6.9 m
power alt
  • 160.0
power main
  • 119.0
span alt
  • 949.96
Manufacturer
  • AEG
max speed main
  • 170.0
engine (prop)
power/mass main
  • 0.100000
climb rate alt
  • 863.380000
empty weight main
  • 800.0
loaded weight alt
  • 2552.0
Developed From
First Flight
  • October 1917
max speed alt
  • 92
jet or prop?
  • prop
empty weight alt
  • 1760.0
plane or copter?
  • plane
Crew
  • Two
Number Built
  • 2
ref
  • German Aircraft of the First World War
abstract
  • The AEG C.VIII was a prototype two-seat reconnaissance aircraft of World War I. Two examples were built, based on the successful C.IV design, one of biplane configuration, the other a triplane (the latter sometimes referred to as the C.VIII.Dr). Neither version offered enough of an improvement on the C.IV to make mass production worthwhile.