{{Short description|1920s German seaplane airliner}} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft | name = V 59/V 61 | logo = | logo_size = | image = LFG V 61.png | alt = | caption = V 61 | long_caption = | other_names = | aircraft_type = Passenger transport | aim = | outcome = | related = | national_origin = Germany | manufacturer = LFG (Luft-Fahrzeug-Gesellschaft) | design_group = | designer = | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 3 (2×V 59 and 1×V 61) | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 1926 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}
The '''LFG V 59''' and the '''LFG V 61''' were single engine, twin float passenger seaplanes designed and built in Germany in 1926 by the Luft-Fahrzeug-Gesellschaft. They differed only in their engines.
==Design and development== The V 59 and V 61 were both twin float seaplanes, essentially identical apart from their engines and designed to carry four or five passengers. The V 59 was powered by a {{convert|240|hp|kW|abbr=on|0}} BMW IV 6-cylinder water cooled inline and the V 61 by a much more powerful, {{convert|400|hp|kW|abbr=on|0}} Bristol Jupiter 9-cylinder radial.<ref name=Flight1/> They were metal aircraft both in frame and covering, low wing monoplanes of the semi-cantilever kind with external bracing between the upper fuselage and wing and further support from below via the flat topped floats. The wings were straight tapered with rounded tips. The fuselage was flat sided and bottomed, with windows down the side and with a braced tailplane mounted on top of it. The rudder extended well below the keel.<ref name=Flight1/>
==Operational history== Both the V 59 and the V 61 were entered into the German Seaplane Competition, held between 12–23 July 1926 with flights along the Baltic and North Sea coasts from Warnemünde.<ref name=Flight1/> The V 59 did not score in the technical tests but the V 61 came sixth in them whilst not completing the whole course.<ref name=Flight2/>
==Variants== ;V 59: {{convert|240|hp|kW|abbr=on|0}} BMW IV 6-cylinder water cooled inline engine. Four passengers. ;V 61: {{convert|400|hp|kW|abbr=on|0}} Bristol Jupiter 9-cylinder radial engine. Estimated maximum speed {{convert|185|km/h|mph|abbr=on|0}}. Five passengers.
==Specifications (V 59)== [[File:LFG V 60 and V 61.png|thumb|The LFG V 61 (foreground) and V 60 (right) at the 1926 German Seaplane Competition]] {{Aircraft specs |ref=Flight 22 July 1926 pp.448-451<ref name=Flight1/> |prime units?=met <!-- General characteristics --> |genhide=
|crew=2 |capacity=4/5 passengers |length m= |length note= |span m= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |lower span m= |lower span ft= |lower span in= |lower span note= |height m= |height ft= |height in= |height note= |wing area sqm=52 |wing area note= |aspect ratio=<!-- give where relevant eg sailplanes --> |airfoil= |empty weight kg=1430 |empty weight note= |gross weight kg=2200 |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=BMW IV |eng1 type=6-cylinder inline water cooled |eng1 hp=240 |eng1 note= |power original= |more power=
|prop blade number= |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note= <!-- Performance --> |perfhide=
|max speed kmh=151 |max speed note= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh=<!-- aerobatic --> |stall speed mph=<!-- aerobatic --> |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |endurance=<!-- if range unknown --> |ceiling m= |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |power/mass=
|more performance= }}
<!-- ==See also== --> {{aircontent <!-- include as many lines are appropriate. additional lines/entries with carriage return. --> |see also= |related=<!-- related developments --> |similar aircraft=<!-- similar or comparable aircraft --> |lists=<!-- related lists --> }}
==References== {{commons category|LFG V 61}} <references>
<ref name=Flight1>{{cite magazine|date=22 July 1926 |title=The German seaplane Championship|magazine=Flight|volume=XVIII|issue=29|pages=448–451|url=http://www.flightglobal.com/pdfarchive/view/1926/1926%20-%200510.html}}</ref>
<ref name=Flight2>{{cite magazine|date=5 August 1926 |title=The German seaplane Championship|magazine=Flight|volume=XVIII|issue=31|page=479|url=http://www.flightglobal.com/pdfarchive/view/1926/1926%20-%200549.html}}</ref>
</references>
{{LFG aircraft}}
Category:Floatplanes Category:1920s German civil aircraft LFG V 59