{{Use dmy dates|date=January 2017}} {{Use British English|date=January 2017}} {{Infobox aircraft | name = Short Biplane No.2 | logo = | logo_size = | image = | alt = | caption = | long_caption = | other_names = | aircraft_type = Experimental aircraft | aim = | outcome = | related = | national_origin = United Kingdom | manufacturer = Short Brothers | design_group = | designer = Horace Short | 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 = 1909 | retired = | first_flight = 27 September 1909 | initiated = | in_service = | last_flight = | expected = | developed_from = | variants = | developed_into = | preservation = | fate = | predecessors = | successors = | concluded = }} The '''Short No.2''' was an early British aircraft built by Short Brothers for J.T.C. Moore-Brabazon. It was used by him to win the £1,000 prize offered by the ''Daily Mail'' newspaper for the first closed-circuit flight of over a mile (1.6 km) to be made in a British aircraft.

==Design and development== The Short No.2 was ordered from Short Brothers in April 1909 with the intention of competing for the £1,000 prize announced by the ''Daily Mail'' for the first closed-circuit flight made by a British aircraft.<ref>Barnes 1967, p.6</ref> The layout of the aircraft was similar to that of the Wright Model A, which the Short Brothers were building under license. It was a biplane with a forward elevator and rear-mounted tailplane, driven by a pair of pusher propellers, chain-driven by the single centrally mounted engine, but differed in a number of significant respects. It was designed to take off using a dolly and launching-rail, like the Wright aircraft, but the landing skids were incorporated into a considerably more substantial structure, each forming the lower member of a trussed girder structure resembling a sleigh, the upturned front end serving to support the biplane front elevators, behind which the rudder was mounted. A single fixed fin was mounted behind the wings on a pair of booms. Lateral control was not effected by wing-warping. Instead it used "balancing planes", each consisting of a pair of low aspect ratio surfaces, mounted at either end of a strut which was pivoted from the midpoint of struts connecting the wingtips.<ref>Barnes 1967, p.45</ref>

==Service history== A {{convert|60|hp|kW|abbr=on}} Green engine had been ordered to power the aircraft, but this had not been delivered when the airframe was completed in September, so an Ateliers Vivinus engine, salvaged from one of Moore-Brabazon's Voisin biplanes, was fitted. Using this engine, a successful flight of nearly a mile was made on 27 September at Shellbeach on the Isle of Sheppey, where both the Short Brother's works and the Royal Aero Club's flying field were located. A second, shorter, flight was made on 4 October, ending in a heavy landing which caused minor damage. While this was being repaired the Green engine was delivered and fitted, but the attempt to win the ''Daily Mail'' prize was delayed by poor weather and did not take place until 30 October, when Moore-Babazon succeeded in rounding a marker post set half a mile from the takeoff point and returning to land next to the launch rail.<ref>Barnes 1967, p.46</ref> A few days later, he responded to a challenge to disprove the saying "pigs can't fly" by making a 3 1/2-mile (5.6&nbsp;km) cross-country flight with a piglet in a basket strapped to one of the interplane struts.

On 7 January it was flown the 4 1/2 miles from Shellbeach to the Royal Aero Club's new flying field at Eastchurch, by which time a revised tail consisting of elongated fixed horizontal and vertical surfaces carried on four booms had been fitted to improve stability. It was now Moore-Brabazon's intention to make an attempt to win the British Empire Michelin Cup, and on 1 March he made a flight covering {{convert|19|mi|km}} in 31 minutes, being forced to land when the engine crankshaft broke.<ref>Barnes 1967 p.47</ref> Although a new engine was fitted, the aircraft was due to be exhibited at the Aero Exhibition at Olympia, and was therefore not flown again until 25 March, by which time it was obvious that nobody else was capable of bettering his flight, and the prize was formally awarded to him. By this time Moore-Brabazon had ordered a new aircraft of the Short S.27 type, and made no subsequent flights in the aircraft.

==Specifications== {{Aircraft specs |ref=<!-- reference --> |prime units?=imp <!-- General characteristics --> |genhide=

|crew=one |capacity= |length m= |length ft=32 |length in=0 |length note= |span m= |span ft=48 |span in=8 |span note= |width note= |height m= |height ft= |height in= |height note= |wing area sqm= |wing area sqft=450 |wing area note= |aspect ratio=<!-- sailplanes --> |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb=1485 |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=Green D.4 |eng1 type=in-line 4-cylinder water-cooled |eng1 kw=<!-- prop engines --> |eng1 hp=60<!-- prop engines --> |eng1 shp=<!-- prop engines --> |eng1 kn=<!-- jet/rocket engines --> |eng1 lbf=<!-- jet/rocket engines --> |eng1 note= |power original= |thrust original=

|prop blade number=2<!-- propeller aircraft --> |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= |max speed mph=45 |max speed kts= |max speed note= |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= |endurance=<!-- if range unknown --> |ceiling m= |ceiling ft= |ceiling note= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |wing loading kg/m2= |wing loading lb/sqft= |wing loading note= |fuel consumption kg/km= |fuel consumption lb/mi= |power/mass= |thrust/weight= |more performance= |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== {{reflist}}

==References== {{refbegin}} *Barnes, C.H. ''Shorts Aircraft Since 1900''. London: Putnam, 1967 {{refend}} <!-- ==External links== -->

{{Short Brothers aircraft}}

Short No.2 biplane Category:1900s British experimental aircraft Category:Single-engined twin-prop pusher aircraft Category:Aircraft first flown in 1909 Category:Biplanes