Albatros G.II: Difference between revisions
m Robot - Moving category German bomber aircraft 1910-1919 to Category:German bomber aircraft 1910–1919 per CFD at Wikipedia:Categories for discussion/Log/2011 September 20. |
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{|{{Infobox Aircraft Begin |
{|{{Infobox Aircraft Begin |
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|name=G.II |
|name=G.II |
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|image=File:Albatros G.II Ray Wagner Collection Image (20822224693).jpg |
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|image= |
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|caption= |
|caption= |
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}}{{Infobox Aircraft Type |
}}{{Infobox Aircraft Type |
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|type= |
|type=Medium bomber |
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|manufacturer=[[Albatros Flugzeugwerke]] |
|manufacturer=[[Albatros Flugzeugwerke]] |
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|designer= |
|designer= |
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|first flight=1916<ref name="Gray">{{cite book|last=Gray|first=Peter|author2=Owen Thetford|title=German Aircraft of the First World War|publisher=Putnam|location=London|year=1970|edition=2nd|isbn=0-370-00103-6}}</ref> |
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|first flight=1916 |
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|introduced= |
|introduced= |
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|retired= |
|retired= |
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|more users= |
|more users= |
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|produced= |
|produced= |
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|number built=1 |
|number built=1<ref name="Gray"/> |
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|variants with their own articles= |
|variants with their own articles= |
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}} |
}} |
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The '''Albatros G.II''' was a [[Germany|German]] [[biplane]] [[bomber]] |
The '''Albatros G.II''', (Company post-war designation L.11), was a twin-engined [[Germany|German]] [[biplane]] [[bomber]] of [[World War I]].<ref name="Gray"/> |
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<!-- ==Development== --> |
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==Development== |
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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.<ref name="Jane's EoA">{{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=53 }}</ref> Only a single prototype was built which demonstrated a relatively poor performance so further development was concentrated on the more powerful [[Albatros G.III]].<ref name="Gray"/> |
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<!-- ==Operational history== --> |
<!-- ==Operational history== --> |
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<!-- ==Variants== --> |
<!-- ==Variants== --> |
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==Operators== |
==Operators== |
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; |
;{{flag|German Empire}} |
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*[[Luftstreitkräfte]] |
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==Specifications (G.II)== |
==Specifications (G.II)== |
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{{Aircraft specs |
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{{aerospecs |
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|ref=German Aircraft of the First World War<ref name="Gray"/> |
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|met or eng?=<!-- eng for US/UK aircraft, met for all others -->met |
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|prime units?=met<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, |
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met(ric) first for all others. You MUST choose a format, or no specifications will show --> |
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<!-- |
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General characteristics |
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--> |
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|genhide=Y |
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|crew= |
|crew= |
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|capacity= |
|capacity= |
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|length ft= |
|length ft= |
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|length in= |
|length in= |
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|length note= |
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|span m= |
|span m= |
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|span ft= |
|span ft= |
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|span in= |
|span in= |
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|span note= |
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|dia m=<!-- helicopters --> |
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|dia ft=<!-- helicopters --> |
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|dia in=<!-- helicopters --> |
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|height m= |
|height m= |
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|height ft= |
|height ft= |
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|height in= |
|height in= |
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|height note= |
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|wing area sqm= |
|wing area sqm= |
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|wing area sqft= |
|wing area sqft= |
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|wing area note= |
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|swept area sqm=<!-- swing-wings --> |
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|swept area sqft=<!-- swing-wings --> |
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|swept area note= |
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|volume m3=<!-- lighter-than-air --> |
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|volume ft3=<!-- lighter-than-air --> |
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|volume note= |
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|aspect ratio=<!-- give where relevant eg sailplanes --> |
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|airfoil= |
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|empty weight kg= |
|empty weight kg= |
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|empty weight lb= |
|empty weight lb= |
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|empty weight note= |
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|gross weight kg= |
|gross weight kg= |
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|gross weight lb= |
|gross weight lb= |
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|gross weight note= |
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|max takeoff weight kg= |
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|max takeoff weight lb= |
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|max takeoff weight note= |
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|fuel capacity= |
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|lift kg=<!-- lighter-than-air --> |
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|lift lb=<!-- lighter-than-air --> |
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|lift note= |
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|more general= |
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<!-- |
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Powerplant |
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--> |
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|eng1 number=2 |
|eng1 number=2 |
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|eng1 |
|eng1 name=[[Benz Bz.III]] |
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|eng1 type=6 cyl. water-cooled in-line piston engine |
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|eng1 kw=<!-- prop engines -->112 |
|eng1 kw=<!-- prop engines -->112 |
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|eng1 hp=<!-- prop engines --> |
|eng1 hp=<!-- prop engines --> |
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|eng1 kn=<!-- jet/rocket engines --> |
|eng1 kn=<!-- jet/rocket engines --> |
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|eng1 lbf=<!-- jet/rocket engines --> |
|eng1 lbf=<!-- jet/rocket engines --> |
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|eng1 note= |
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|power original= |
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|thrust original= |
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|eng1 kn-ab=<!-- afterburners --> |
|eng1 kn-ab=<!-- afterburners --> |
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|eng1 lbf-ab=<!-- afterburners --> |
|eng1 lbf-ab=<!-- afterburners --> |
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|eng2 number= |
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|eng2 number=<!-- for different engine types --> |
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|eng2 name= |
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|eng2 type= |
|eng2 type= |
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|eng2 kw=<!-- prop engines --> |
|eng2 kw=<!-- prop engines --> |
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|eng2 kn=<!-- jet/rocket engines --> |
|eng2 kn=<!-- jet/rocket engines --> |
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|eng2 lbf=<!-- jet/rocket engines --> |
|eng2 lbf=<!-- jet/rocket engines --> |
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|eng2 note= |
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|eng2 kn-ab=<!-- afterburners --> |
|eng2 kn-ab=<!-- afterburners --> |
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|eng2 lbf-ab=<!-- afterburners --> |
|eng2 lbf-ab=<!-- afterburners --> |
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|eng3 number=<!-- for different engine types --> |
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|eng3 name= |
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|eng3 type= |
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|eng3 kw=<!-- prop engines --> |
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|eng3 hp=<!-- prop engines --> |
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|eng3 kn=<!-- jet/rocket engines --> |
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|eng3 lbf=<!-- jet/rocket engines --> |
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|eng3 note= |
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|eng3 kn-ab=<!-- afterburners --> |
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|eng3 lbf-ab=<!-- afterburners --> |
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|more power= |
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|prop blade number=<!-- propeller aircraft --> |
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|prop name= |
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|prop dia m=<!-- propeller aircraft --> |
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|prop dia ft=<!-- propeller aircraft --> |
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|prop dia in=<!-- propeller aircraft --> |
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|prop note= |
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|rot number=<!-- helicopters --> |
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|rot dia m=<!-- helicopters --> |
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|rot dia ft=<!-- helicopters --> |
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|rot dia in=<!-- helicopters --> |
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|rot area sqm=<!-- helicopters --> |
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|rot area sqft=<!-- helicopters --> |
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|rot area note= |
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<!-- |
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Performance |
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--> |
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|perfhide=Y |
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|max speed kmh= |
|max speed kmh= |
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|max speed mph= |
|max speed mph= |
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|max speed kts= |
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|max speed note= |
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|max speed mach=<!-- supersonic aircraft --> |
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|cruise speed kmh= |
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|cruise speed mph= |
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|cruise speed kts= |
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|cruise speed note= |
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|stall speed kmh=<!-- aerobatic --> |
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|stall speed mph=<!-- aerobatic --> |
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|stall speed kts= |
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|stall speed note= |
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|never exceed speed kmh= |
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|never exceed speed mph= |
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|never exceed speed kts= |
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|never exceed speed note= |
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|minimum control speed kmh= |
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|minimum control speed mph= |
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|minimum control speed kts= |
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|minimum control speed note= |
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|range km= |
|range km= |
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|range miles= |
|range miles= |
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|range nmi= |
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|endurance h=<!-- if range unknown --> |
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|range note= |
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|endurance min=<!-- if range unknown --> |
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|combat range km= |
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|combat range miles= |
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|combat range nmi= |
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|combat range note= |
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|ferry range km= |
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|ferry range miles= |
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|ferry range nmi= |
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|ferry range note= |
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|endurance=<!-- if range unknown --> |
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|ceiling m= |
|ceiling m= |
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|ceiling ft= |
|ceiling ft= |
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|ceiling note= |
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|g limits=<!-- aerobatic --> |
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|roll rate=<!-- aerobatic --> |
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|glide ratio=<!-- sailplanes --> |
|glide ratio=<!-- sailplanes --> |
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|climb rate ms= |
|climb rate ms= |
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|climb rate ftmin= |
|climb rate ftmin= |
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|climb rate note= |
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|time to altitude= |
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|sink rate ms=<!-- sailplanes --> |
|sink rate ms=<!-- sailplanes --> |
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|sink rate ftmin=<!-- sailplanes --> |
|sink rate ftmin=<!-- sailplanes --> |
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|sink rate note= |
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|armament1= |
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|lift to drag= |
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|armament2= |
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|wing loading kg/m2= |
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|armament3= |
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|wing loading lb/sqft= |
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|armament4= |
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|wing loading note= |
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|armament5= |
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|disk loading kg/m2= |
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|armament6= |
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|disk loading lb/sqft= |
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|disk loading note= |
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|power/mass= |
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|thrust/weight= |
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|more performance= |
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<!-- |
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Armament |
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--> |
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|guns= |
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|bombs= |
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|avionics= |
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}} |
}} |
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|related=<!-- related developments --> |
|related=<!-- related developments --> |
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|similar aircraft=<!-- similar or comparable aircraft --> |
|similar aircraft=<!-- similar or comparable aircraft --> |
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*[[A.E.G. G.I]] |
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|lists=<!-- related lists --> |
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*[[Daimler R.I]] |
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*[[Union G.I]] |
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|lists= |
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|see also=<!-- other relevant information --> |
|see also=<!-- other relevant information --> |
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}} |
}} |
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==References== |
==References== |
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{{commons category}} |
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* {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |
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|year=1989 |publisher=Studio Editions |location=London |pages=53 }} |
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<!-- ==External links== --> |
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===Notes=== |
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{{wwi-air}} |
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{{Reflist}} |
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{{Idflieg G-class designations}} |
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{{aviation lists}} |
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===Bibliography=== |
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*{{cite book |last1=Herris |first1=Jack |title=Albatros Aircraft of WWI: A Centennial Perspective on Great War Airplanes: Volume 3: Bombers, Seaplanes, J-Types |date=2017 |publisher=Aeronaut Books |location=Charleston, South Carolina |isbn=978-1-935881-49-0|series=Great War Aviation Centennial Series |volume=26}} |
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*{{cite journal|last=S|first=W|title=Rara Avis - The Albatros G.II/G.III|journal=Windsock Worldwide|date=September–October 2009|volume=25|issue=5 |publisher=Albatros Productions |pages=12–14}} |
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<!-- ==External links== --> |
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{{Albatros aircraft}} |
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{{Idflieg G, GL, K, L and N-class designations}} |
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[[Category:Albatros aircraft|G.II]] |
[[Category:Albatros aircraft|G.II]] |
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[[Category:German bomber aircraft |
[[Category:1910s German bomber aircraft]] |
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[[Category:Aircraft first flown in 1916]] |
Latest revision as of 11:07, 21 April 2024
G.II | |
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![]() | |
Role | Medium bomber |
Manufacturer | Albatros Flugzeugwerke |
First flight | 1916[1] |
Primary user | Deutschland |
Number built | 1[1] |
The Albatros G.II, (Company post-war designation L.11), was a twin-engined German biplane bomber of World War I.[1]
Development
[edit]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.[2] Only a single prototype was built which demonstrated a relatively poor performance so further development was concentrated on the more powerful Albatros G.III.[1]
Operators
[edit]Specifications (G.II)
[edit]Data from German Aircraft of the First World War[1]
- Powerplant: 2 × Benz Bz.III 6 cyl. water-cooled in-line piston engine, 112 kW (150 hp) each
See also
[edit]Aircraft of comparable role, configuration, and era
References
[edit]![](http://upload.wikimedia.org/wikipedia/en/thumb/4/4a/Commons-logo.svg/30px-Commons-logo.svg.png)
Notes
[edit]Bibliography
[edit]- 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. ISBN 978-1-935881-49-0.
- S, W (September–October 2009). "Rara Avis - The Albatros G.II/G.III". Windsock Worldwide. 25 (5). Albatros Productions: 12–14.