About: Speedtwin E2E Comet 1

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The Speedtwin E2E Comet 1, originally named the Phillips ST1 Speedtwin, is a two-seat, twin engined aircraft designed in the UK to be capable of aerobatics and the only civil twin certified for intentional spinning. After a long development time, just two have been built.

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rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft settlement yago:Type105840188
rdfs:label	Speedtwin E2E Comet 1 (en)
rdfs:comment	The Speedtwin E2E Comet 1, originally named the Phillips ST1 Speedtwin, is a two-seat, twin engined aircraft designed in the UK to be capable of aerobatics and the only civil twin certified for intentional spinning. After a long development time, just two have been built. (en)
foaf:depiction
dct:subject	1990s British sport aircraft Low-wing aircraft Aircraft first flown in 1991 Twin piston-engined tractor aircraft
Wikipage page ID	40881112 (xsd:integer)
Wikipage revision ID	1049625460 (xsd:integer)
Link from a Wikipage to another Wikipage	NACA airfoil Monoplane Victa Airtourer Conventional undercarriage De Havilland Canada DHC-1 Chipmunk Inline engine (aeronautics) Elevator (aircraft) Wing tip Oleo strut 1990s British sport aircraft Lycoming IO-390 Composite material Tandem Low-wing aircraft UK Fuselage Leading edge Aerobatic Ailerons Aircraft canopy Aircraft fairing Farnborough Airshow Balanced rudder Monocoque Trailing edge Hydraulic brake Flap (aircraft) Aircraft first flown in 1991 Twin piston-engined tractor aircraft Cockpit Avia M 332 Fillet (mechanics) Cantilever Rudder Dihedral (aircraft) Flat four Turbo-prop Flat four engine Continental O-200-A
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sameAs	Speedtwin E2E Comet 1 Speedtwin E2E Comet 1 Speedtwin E2E Comet 1
span m	7.920000 (xsd:double)
stall speed kmh	120 (xsd:integer)
wing area sqm	11.400000 (xsd:double)
wing loading kg/m	79.700000 (xsd:double)
wing loading note	at maximum aerobatic weight (en)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Convert dbt:Reflist dbt:Use_British_English dbt:Use_dmy_dates dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/Phillips_ST2_Speedtwin.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	1991-09-30 (xsd:date)
national origin	UK
capacity	Two (en)
designer	Peter John Croft Phillips (en)
fuel capacity	400.0 (litre)
manufacturer	Speedtwin Developments Ltd (en)
ref	Jane's All the World's Aircraft 2013–14, pp. 672–3 (en)
type	Two seat aerobatic twin (en)
has abstract	The Speedtwin E2E Comet 1, originally named the Phillips ST1 Speedtwin, is a two-seat, twin engined aircraft designed in the UK to be capable of aerobatics and the only civil twin certified for intentional spinning. After a long development time, just two have been built. (en)
airfoil	NACA 23012, with washout to NACA 2412 outboard (en)
climb rate ms	10.200000 (xsd:double)
climb rate note	73200.0 (second)
empty weight kg	680 (xsd:integer)
eng1 kw	153 (xsd:integer)
eng1 name	Titan/Lycoming IO-390 (en)

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