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AEG B.III

From Biocrawler, the free encyclopedia.

The AEG B.III was a two-seat biplane reconnaissance aircraft produced in very small numbers from 1915. It was a further refinement of the B.I and B.II but was still only just adequate in performance and did not attract much interest.

Contents

Specifications (AEG B.III)

General Characteristics

  • Crew: two, pilot and observer
  • Length: 7.9 m (25 ft 11 in)
  • Wingspan: 13.1 m (43 ft)
  • Height: m ( ft in)
  • Wing area: 41 m² (441 ft²)
  • Empty: kg ( lb)
  • Loaded: kg ( kg)
  • Maximum takeoff: kg ( lb)
  • Powerplant: 1x Mercedes D.II, 88 kW (118 hp)

Performance

  • Maximum speed: 110 km/h (176 mph)
  • Range: km ( miles)
  • Service ceiling: m ( ft)
  • Rate of climb: m/min ( ft/min)
  • Wing loading: kg/m² ( lb/ft²)
  • Power/Mass: kW/kg ( hp/lb)

Related content

Related development:

Comparable aircraft:

Designation sequence: AEG B.I - AEG B.II - AEG B.III


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Wikipedia (http://en.wikipedia.org/wiki/Main_Page) AEG_B.III (http://en.wikipedia.org/wiki/AEG_B.III) version history (http://en.wikipedia.org/w/index.php?title=AEG_B.III&action=history) GNU Free Documentation Lizenz (http://en.wikipedia.org/wiki/Wikipedia:Text_of_the_GNU_Free_Documentation_License) CC-by-sa (http://creativecommons.org/licenses/by-sa/2.5/)

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