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Designed as a medium bomber, the G.II did not share any attributes with the larger G.I, being a single bay biplane with thick section upper wings and rigid X member inter-plane struts. The graceful lines of the fuselage were spoilt by the twin nose-wheel assembly, intended to reduce damage on nose-overs and at rest with a forward centre of gravity. A conventional tail-unit terminated the rear fuselage. The engines were installed in pusher nacelles, supported by struts from the fuselage and the lower wing trailing edges had cut-outs to allow the engines to be mounted further forward than otherwise possible. Only a single prototype was built which demonstrated a relatively poor performance so further development was concentrated on the more powerful Albatros G.III.
^ Gray, Peter; Owen Thetford (1970). German Aircraft of the First World War (2nd ed.). London: Putnam. ISBN0-370-00103-6.
Taylor, Michael J. H. (1989). Jane's Encyclopedia of Aviation. London: Studio Editions. p. 53.
Bibliography
Herris, Jack (2017). Albatros Aircraft of WWI: A Centennial Perspective on Great War Airplanes: Volume 3: Bombers, Seaplanes, J-Types. Great War Aviation Centennial Series. Vol. 26. Charleston, South Carolina: Aeronaut Books. ISBN978-1-935881-49-0.
S, W (September–October 2009). "Rara Avis - The Albatros G.II/G.III". Windsock Worldwide. 25 (5). Albatros Productions: 12–14.