About: Lambert Mission 212

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An Entity of Type : yago:Type105840188, within Data Space : dbpedia.org associated with source document(s)
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The Lambert Mission 212 is a conventionally laid out low-wing, fixed undercarriage, single-engine, four-seat kit built aircraft designed in the UK by a Belgian college student. Kits are manufactured in Belgium.

Attributes	Values
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 yago:Type105840188
rdfs:label	Lambert Mission 212 (en)
rdfs:comment	The Lambert Mission 212 is a conventionally laid out low-wing, fixed undercarriage, single-engine, four-seat kit built aircraft designed in the UK by a Belgian college student. Kits are manufactured in Belgium. (en)
dcterms:subject	2000s Belgian aircraft
Wikipage page ID	34255261 (xsd:integer)
Wikipage revision ID	993816155 (xsd:integer)
Link from a Wikipage to another Wikipage	Royal Aeronautical Society Belgium Homebuilt aircraft Elevator (aircraft) Pre-preg Epoxy resin Low-wing Lycoming O-320 Lycoming O-360 Composite material 2000s Belgian aircraft Popular Flying Association UK Wevelgem Fuselage College of Aeronautics, Cranfield Lambert Mission 106 Aircraft canopy Fin Balanced rudder DeltaHawk DH180A4 Monocoque Dorsal (anatomy) Trailing edge Flap (aircraft) Chord (aircraft) Landing gear Tailplane Diesel engine Philippines Fairing (aircraft) Netherlands Cantilever Rudder Dihedral (aircraft) Spar (aviation) Zoche aero-diesel Two-stroke Carbon fibre Washout (aviation) Flat-four Glass fibre Superior XP-360 Wingtip dbr:Superior_X-360
sameAs	Lambert Mission 212 Lambert Mission 212 Lambert Mission 212
span m	9.800000 (xsd:double)
stall speed kmh	99 (xsd:integer)
stall speed note	flaps down (en)
wing area sqm	12 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs
dbp:primeUnits%3F_	met (en)
first flight	2004-07-13 (xsd:date)
capacity	three (en)
crew	one (en)
fuel capacity	160 (xsd:integer)
manufacturer	Lambert Aircraft Engineering BVBA, Wevelgem (en)
ref	Jane's All the World's Aircraft 2011/12 (en)
type	Four-seat kit built (en)
unit cost	59900.0 (euro) kit, excluding engine, propeller and avionics (en)
has abstract	The Lambert Mission 212 is a conventionally laid out low-wing, fixed undercarriage, single-engine, four-seat kit built aircraft designed in the UK by a Belgian college student. Kits are manufactured in Belgium. (en)
aspect ratio	8 (xsd:integer)
climb rate ms	4.600000 (xsd:double)
climb rate note	maximum at sea level (en)
cruise speed kmh	233 (xsd:integer)
cruise speed note	at 60% power (en)
empty weight kg	722 (xsd:integer)
eng1 kw	134 (xsd:integer)
eng1 name	Superior XP-360
eng1 number	1 (xsd:integer)
eng1 type	Flat-four
height m	2.900000 (xsd:double)
length m	7.400000 (xsd:double)
max speed kmh	259 (xsd:integer)
max takeoff weight kg	1150 (xsd:integer)

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