{{Short description|Prototype American military aircraft of 1914 }} {{About |a prototype military aircraft built by the Wright Company in 1914 |the Wright aircraft design built under licence by the Burgess Company as the Model F |Wright Model B}} {{Use mdy dates |date=April 2025 }} {{Use American English|date=April 2025 }} <!-- This article is a part of Wikipedia:WikiProject Aircraft. Please see Wikipedia:WikiProject Aircraft/page content for recommended layout. --> {{Infobox aircraft | name = Model F | logo = | logo_size = | image = File:Wright Model F.jpg | alt = | caption = | long_caption = | other_names = | aircraft_type = Military reconnaissance aircraft | aim = | outcome = | related = | national_origin = United States | manufacturer = Wright Company | design_group = | designer = Grover Loening | builder = | issuer = | status = | owners = | primary_user = | more_users = | service = | major_applications = | proposals = | prototypes = | number_built = 1 | construction_number = | civil_registration = | military_serial = | radio_code = | requirement = | aircraft_carried = | flights = | total_hours = | total_distance = | construction_date = | introduction = | retired = | first_flight = 1914 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }}
The '''Wright Model F''' was a prototype military aircraft built by the Wright Company for the U.S. Army in 1914. It was the first Wright design to feature a fuselage.<ref name="jea">Taylor 1992, p.898</ref><ref name="iea">''The Illustrated Encyclopedia of Aircraft'' 1985, p.3098</ref><ref name="flight">"The New Wright Biplane" 1914, p.1133</ref><ref name="roach104">Roach 2016, p.104</ref> The major structural elements of previous Wright designs had been connected by open frameworks.<ref name="swanborough478">Swanborough 1963, p.478</ref> The application of metal armor to the underside of the fuselage, together with its unenviable performance,<ref name="hallion68">Hallion 2019, p.68</ref> earned the aircraft the nickname "'''Tin Cow'''".
==Design== The Model F was a three-bay, unstaggered biplane with equal-span wings. Its overall configuration was conventional, with a conventional tail carried at the rear of the fuselage.<ref name="flight"/> The pilot and observer sat side-by-side in an open cockpit.<ref name="flight"/> Power was supplied by a piston engine mounted in the nose, which drove two two-bladed pusher propellers mounted on the interplane struts and linked by chain drives.<ref name="flight"/> It was fitted with fixed, tailskid undercarriage.<ref name="flight"/>
==Development== The Model F was designed in response to a 1913 U.S. Army Signal Corps specification for a reconnaissance aircraft.<ref name="hallion67">Hallion 2019, p.67</ref> The specification called for the underside of the aircraft to carry a crew of two with a four-hour endurance, be protected by chrome-steel armor, and to be capable of carrying a machine gun.<ref name="hallion67"/> Due to a lack of confidence in American-produced aero engines of the time, the specification also called for use of a foreign powerplant.<ref name="hallion67"/> The contract was worth $9,500.<ref name="roach104"/>
Wright responded with a design by Grover Loening that resembled the contemporary French designs,<ref name="roach104"/><ref name="hallion6768">Hallion 2019, p.67–68</ref> with a fuselage, and tail unit that consisted of a fin and horizontal stabilizer. Loenig also adopted the current "Deperdussin-style" controls that combined the aircraft's controls into a central control stick.<ref name="hallion68"/> As originally designed, the aircraft was powered by tractor propellers.<ref name="hallion67"/>
A series of revisions followed, which aviation historian Richard P. Hallion describes as "a dark comedy of errors".<ref name="hallion68"/> At one stage of development, the aircraft was equipped both with "Deperdussin-style" controls, as well as the system of control wheels fitted to previous Wright designs, before the "Deperdussin-style" controls were removed completely.<ref name="hallion68"/> The tractor propellers were moved to become pushers, and the seating arrangement was changed to be side-by-side.<ref name="hallion68"/>
By the time the Model F was finally delivered, it was already a year late, Wright was delivering it at a financial loss, and Loening had quit the company in frustration.<ref name="hallion68"/>
==Operational history== The Model F was accepted by the Army in March 1915, and given the serial number "39".<ref name="swanborough478"/><ref name="hallion68"/> During testing it was described as "a lumbersome mass of rattling material" and given its "Tin Cow" nickname.<ref name="hallion68"/> Test pilot Lt. Herbert Dargue said that it was "uncontrollable on the ground and out of date."<ref name="roach105">Roach 2015, p.105</ref> Only two months later, the aircraft was withdrawn<ref name="roach105"/><ref name="hallion68"/> along with all the Army's other pusher designs.<ref name="roach105"/> It had only flown seven times.<ref name="roach105"/>
<!-- ==Variants== --> ==Operators== * United States Army Signal Corps
==Specifications== {{Aircraft specs |ref=<!-- reference -->Hallion 2019, p.68 |prime units?=<!-- imp or kts first for US aircraft, and UK aircraft pre-metrification, met(ric) first for all others. You MUST choose a format, or no specifications will show -->imp <!-- General characteristics --> |genhide=
|crew=2 |capacity= |length m= |length ft=32 |length in=10 |length note= |span m= |span ft=42 |span in=0 |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m=<!-- swing-wings --> |swept ft=<!-- swing-wings --> |swept in=<!-- swing-wings --> |swept note= |dia m=<!-- airships etc --> |dia ft=<!-- airships etc --> |dia in=<!-- airships etc --> |dia note= |width m=<!-- if applicable --> |width ft=<!-- if applicable --> |width in=<!-- if applicable --> |width note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft=485 |wing area note=(estimated) |swept area sqm=<!-- swing-wings --> |swept area sqft=<!-- swing-wings --> |swept area note= |volume m3=<!-- lighter-than-air --> |volume ft3=<!-- lighter-than-air --> |volume note= |aspect ratio=<!-- sailplanes --> |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg=<!-- lighter-than-air --> |lift lb=<!-- lighter-than-air --> |lift note= |more general= <!-- Powerplant --> |eng1 number=1 |eng1 name=Beardmore-built Austro-Daimler |eng1 type=six-cylinder, water-cooled, inline piston engine |eng1 kw=<!-- prop engines --> |eng1 hp=<!-- prop engines -->90 |eng1 shp=<!-- prop engines --> |eng1 kn=<!-- jet/rocket engines --> |eng1 lbf=<!-- jet/rocket engines --> |eng1 note= |power original= |thrust original= |eng1 kn-ab=<!-- afterburners --> |eng1 lbf-ab=<!-- afterburners -->
|eng2 number= |eng2 name= |eng2 type= |eng2 kw=<!-- prop engines --> |eng2 hp=<!-- prop engines --> |eng2 shp=<!-- prop engines --> |eng2 kn=<!-- jet/rocket engines --> |eng2 lbf=<!-- jet/rocket engines --> |eng2 note= |eng2 kn-ab=<!-- afterburners --> |eng2 lbf-ab=<!-- afterburners -->
|eng3 number= |eng3 name= |eng3 type= |eng3 kw=<!-- prop engines --> |eng3 hp=<!-- prop engines --> |eng3 shp=<!-- prop engines --> |eng3 kn=<!-- jet/rocket engines --> |eng3 lbf=<!-- jet/rocket engines --> |eng3 note= |eng3 kn-ab=<!-- afterburners --> |eng3 lbf-ab=<!-- afterburners --> |more power=
|prop blade number=<!-- propeller aircraft --> |prop name= |prop dia m=<!-- propeller aircraft --> |prop dia ft=<!-- propeller aircraft --> |prop dia in=<!-- propeller aircraft --> |prop dia note=
|rot number=<!-- helicopters --> |rot dia m=<!-- helicopters --> |rot dia ft=<!-- helicopters --> |rot dia in=<!-- helicopters --> |rot area sqm=<!-- helicopters --> |rot area sqft=<!-- helicopters --> |rot area note= <!-- Performance --> |perfhide=
|max speed kmh= |max speed mph=60 |max speed kts= |max speed note=(estimated) |max speed mach=<!-- supersonic aircraft --> |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |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= |combat range km= |combat range miles= |combat range nmi= |combat range note= |ferry range km= |ferry range miles= |ferry range nmi= |ferry range note= |endurance=<!-- if range unknown --> |ceiling m= |ceiling ft= |ceiling note= |g limits=<!-- aerobatic --> |roll rate=<!-- aerobatic --> |glide ratio=<!-- sailplanes --> |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms=<!-- sailplanes --> |sink rate ftmin=<!-- sailplanes --> |sink rate note= |lift to drag= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |thrust/weight=
|more performance= <!-- Armament --> |armament=<!-- add bulletted list here or if you want to use the following specific parameters, remove this parameter--> |guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other=
|avionics= }}
<!-- ==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 --> }}
==Notes== {{Commons category}} ===References=== {{reflist}}
===Bibliography=== <!-- these are only examples of some commonly-cited works; add and remove as needed! --> * {{cite book |last=Hallion |first=Richard P. |title=The Wright Flyers 1899–1916 |publisher=Osprey |location=Oxford |year=2019 }} * {{cite book |title=The Illustrated Encyclopedia of Aircraft |publisher=Aerospace Publishing|location=London }} * {{cite journal |title=The New Wright Biplane |journal=Flight |publisher=Flight |location=London |volume=6 |number=47 |date=November 20, 1914 |page=1133 }} * {{cite book |last=Roach |first=Edward J. |title=The Wright Company: From Invention to Industry |publisher=Ohio University Press |location=Athens, OH |year=2014 }} * {{cite book |last=Swanborough |first=Gordon |title=United States Military Aircraft Since 1909 |publisher=Putnam |location=London |year=1963 }} * {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1993 |publisher=Studio Editions |location=London }}
<!-- ==External links== --> {{Wright aircraft}}
Category:1910s United States military reconnaissance aircraft<!-- decade-country-role category --> Category:Wright aircraft<!-- manufacturer category --> Category:Biplanes<!-- wing configuration category--> Category:Conventional-tail aircraft<!-- tail category--> Category:Single-engined twin-prop pusher aircraft<!-- engine configuration category --> Category:Aircraft with fixed conventional landing gear<!-- undercarriage category --> Category:Aircraft first flown in 1914<!-- first flight category -->