Matches in DBpedia 2016-04 for { <http://dbpedia.org/resource/Lambert_Mission_212> ?p ?o }
- Lambert_Mission_212 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.".
- Lambert_Mission_212 manufacturer Wevelgem.
- Lambert_Mission_212 numberBuilt "2".
- Lambert_Mission_212 type Homebuilt_aircraft.
- Lambert_Mission_212 unitCost "59900.0".
- Lambert_Mission_212 wikiPageID "34255261".
- Lambert_Mission_212 wikiPageLength "8546".
- Lambert_Mission_212 wikiPageOutDegree "47".
- Lambert_Mission_212 wikiPageRevisionID "668325766".
- Lambert_Mission_212 wikiPageWikiLink Aircraft_canopy.
- Lambert_Mission_212 wikiPageWikiLink Aircraft_fairing.
- Lambert_Mission_212 wikiPageWikiLink Anatomical_terms_of_location.
- Lambert_Mission_212 wikiPageWikiLink Balanced_rudder.
- Lambert_Mission_212 wikiPageWikiLink Belgium.
- Lambert_Mission_212 wikiPageWikiLink Cantilever.
- Lambert_Mission_212 wikiPageWikiLink Carbon-fiber-reinforced_polymer.
- Lambert_Mission_212 wikiPageWikiLink Category:Belgian_aircraft_2000–2009.
- Lambert_Mission_212 wikiPageWikiLink Chord_(aeronautics).
- Lambert_Mission_212 wikiPageWikiLink Composite_material.
- Lambert_Mission_212 wikiPageWikiLink Cranfield_University.
- Lambert_Mission_212 wikiPageWikiLink DeltaHawk_DH180A4.
- Lambert_Mission_212 wikiPageWikiLink Diesel_engine.
- Lambert_Mission_212 wikiPageWikiLink Dihedral_(aeronautics).
- Lambert_Mission_212 wikiPageWikiLink Elevator_(aeronautics).
- Lambert_Mission_212 wikiPageWikiLink Epoxy.
- Lambert_Mission_212 wikiPageWikiLink Fin.
- Lambert_Mission_212 wikiPageWikiLink Flap_(aeronautics).
- Lambert_Mission_212 wikiPageWikiLink Flat-four_engine.
- Lambert_Mission_212 wikiPageWikiLink Fuselage.
- Lambert_Mission_212 wikiPageWikiLink Glass_fiber.
- Lambert_Mission_212 wikiPageWikiLink Homebuilt_aircraft.
- Lambert_Mission_212 wikiPageWikiLink Lambert_Mission_106.
- Lambert_Mission_212 wikiPageWikiLink Landing_gear.
- Lambert_Mission_212 wikiPageWikiLink Light_Aircraft_Association.
- Lambert_Mission_212 wikiPageWikiLink Lycoming_O-320.
- Lambert_Mission_212 wikiPageWikiLink Lycoming_O-360.
- Lambert_Mission_212 wikiPageWikiLink Monocoque.
- Lambert_Mission_212 wikiPageWikiLink Monoplane.
- Lambert_Mission_212 wikiPageWikiLink Netherlands.
- Lambert_Mission_212 wikiPageWikiLink Philippines.
- Lambert_Mission_212 wikiPageWikiLink Pre-preg.
- Lambert_Mission_212 wikiPageWikiLink Royal_Aeronautical_Society.
- Lambert_Mission_212 wikiPageWikiLink Rudder.
- Lambert_Mission_212 wikiPageWikiLink Spar_(aeronautics).
- Lambert_Mission_212 wikiPageWikiLink Superior_X-360.
- Lambert_Mission_212 wikiPageWikiLink Superior_XP-360.
- Lambert_Mission_212 wikiPageWikiLink Tailplane.
- Lambert_Mission_212 wikiPageWikiLink Trailing_edge.
- Lambert_Mission_212 wikiPageWikiLink Two-stroke_engine.
- Lambert_Mission_212 wikiPageWikiLink United_Kingdom.
- Lambert_Mission_212 wikiPageWikiLink Washout_(aeronautics).
- Lambert_Mission_212 wikiPageWikiLink Wevelgem.
- Lambert_Mission_212 wikiPageWikiLink Wing_tip.
- Lambert_Mission_212 wikiPageWikiLink Zoche_aero-diesel.
- Lambert_Mission_212 wikiPageWikiLinkText "Lambert Mission 212".
- Lambert_Mission_212 aspectRatio "8".
- Lambert_Mission_212 capacity "three".
- Lambert_Mission_212 climbRateMs "4.6".
- Lambert_Mission_212 climbRateNote "maximum at sea level".
- Lambert_Mission_212 crew "one".
- Lambert_Mission_212 cruiseSpeedKmh "233".
- Lambert_Mission_212 cruiseSpeedNote "at 60% power".
- Lambert_Mission_212 emptyWeightKg "722".
- Lambert_Mission_212 eng1Kw "134".
- Lambert_Mission_212 eng1Name Superior_XP-360.
- Lambert_Mission_212 eng1Number "1".
- Lambert_Mission_212 eng1Type Flat-four_engine.
- Lambert_Mission_212 firstFlight "2004-07-13".
- Lambert_Mission_212 fuelCapacity "160".
- Lambert_Mission_212 heightM "2.9".
- Lambert_Mission_212 lengthM "7.4".
- Lambert_Mission_212 manufacturer "Lambert Aircraft Engineering BVBA, Wevelgem".
- Lambert_Mission_212 maxSpeedKmh "259".
- Lambert_Mission_212 maxTakeoffWeightKg "1150".
- Lambert_Mission_212 morePerformance "16800.0".
- Lambert_Mission_212 neverExceedSpeedKmh "338".
- Lambert_Mission_212 numberBuilt "2".
- Lambert_Mission_212 primeUnits%3F_ "met".
- Lambert_Mission_212 propBladeNumber "3".
- Lambert_Mission_212 rangeKm "1018".
- Lambert_Mission_212 rangeNote "maximum fuel, 60% power".
- Lambert_Mission_212 ref "Jane's All the World's Aircraft 2011/12".
- Lambert_Mission_212 spanM "9.8".
- Lambert_Mission_212 stallSpeedKmh "99".
- Lambert_Mission_212 stallSpeedNote "flaps down".
- Lambert_Mission_212 type "Four-seat kit built".
- Lambert_Mission_212 unitCost "59900.0".
- Lambert_Mission_212 unitCost "kit, excluding engine, propeller and avionics".
- Lambert_Mission_212 wikiPageUsesTemplate Template:Aircontent.
- Lambert_Mission_212 wikiPageUsesTemplate Template:Aircraft_specs.
- Lambert_Mission_212 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- Lambert_Mission_212 wikiPageUsesTemplate Template:Reflist.
- Lambert_Mission_212 wingAreaSqm "12".
- Lambert_Mission_212 subject Category:Belgian_aircraft_2000–2009.
- Lambert_Mission_212 type Aircraft.
- Lambert_Mission_212 type MeanOfTransportation.
- Lambert_Mission_212 type Product.
- Lambert_Mission_212 type DesignedArtifact.
- Lambert_Mission_212 type Thing.
- Lambert_Mission_212 type Q11436.