Thulin L
{{short description|1910s Swedish aircraft}}
| {{Infobox Aircraft Begin
| name= Type L | image= | caption= }}{{Infobox Aircraft Type | type=Reconnaissance aircraft | manufacturer=AB Thulinverken | designer=Enoch Thulin | first flight= April 1916 | introduced= | retired= | status= | primary user= Swedish Air Force | more users= | produced= | number built=5 | variants with their own articles=Thulin LA }} |
The Thulin L was a Swedish reconnaissance plane built in the late 1910s.
Design and development
The Thulin L was a two-seat biplane derived from the unsuccessful Thulin E. It differed from the latter in that the wing surface was increased and the float location was made easier. Four production Thulin L floatplanes were ordered July 4, 1916, and they were delivered from November 1916 to March 1917.
Specifications
{{Aircraft specs
|prime units?=met
|crew=2
|capacity=
|length m=7.5
|span m=11.6
|upper span m=
|mid span m=
|lower span m=
|width m=
|height m=3.52
|wing area sqm=36.5
|aspect ratio=
|airfoil=
|empty weight kg=
|gross weight kg=965
|max takeoff weight kg=
|fuel capacity=
|more general=
|eng1 number=1
|eng1 name=Thulin A
|eng1 type=9-cylinder air-cooled rotary piston engine
|eng1 hp=90
|prop blade number=
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|perfhide=
|max speed kmh=120
|max speed mach=
|cruise speed kmh=95
|stall speed kmh=
|never exceed speed kmh=
|minimum control speed kmh=
|range km=
|combat range km=
|ferry range km=
|endurance=
|ceiling m=
|g limits=
|roll rate=
|climb rate ms=
|time to altitude=
|wing loading kg/m2=
|fuel consumption kg/km=
|power/mass=
|thrust/weight=
|more performance=
|guns=
|bombs=
|rockets=
|missiles=
|hardpoints=
|hardpoint capacity=
|hardpoint rockets=
|hardpoint missiles=
|hardpoint bombs=
|hardpoint other=
|avionics=
}}
See also
{{aircontent|
|related=
|similar aircraft=
|lists=
|see also=
}}
References
{{Reflist}}
{{Thulin aircraft}}
Category:Single-engined tractor aircraft
Category:1910s Swedish aircraft