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- Rotorvox_C2A abstract "The Rotorvox C2A is a two seat, pusher configuration autogyro developed in Germany.".
- Rotorvox_C2A origin Germany.
- Rotorvox_C2A type Autogyro.
- Rotorvox_C2A wikiPageID "46998698".
- Rotorvox_C2A wikiPageLength "4392".
- Rotorvox_C2A wikiPageOutDegree "26".
- Rotorvox_C2A wikiPageRevisionID "668369914".
- Rotorvox_C2A wikiPageWikiLink Aircraft_canopy.
- Rotorvox_C2A wikiPageWikiLink Aircraft_fairing.
- Rotorvox_C2A wikiPageWikiLink Aluminium.
- Rotorvox_C2A wikiPageWikiLink Anatomical_terms_of_location.
- Rotorvox_C2A wikiPageWikiLink Autogyro.
- Rotorvox_C2A wikiPageWikiLink Canopy_(aircraft).
- Rotorvox_C2A wikiPageWikiLink Carbon-fiber-reinforced_polymer.
- Rotorvox_C2A wikiPageWikiLink Carbon-fibre.
- Rotorvox_C2A wikiPageWikiLink Category:Autogyros.
- Rotorvox_C2A wikiPageWikiLink Category:German_aircraft_2000–2009.
- Rotorvox_C2A wikiPageWikiLink Fin.
- Rotorvox_C2A wikiPageWikiLink Flat-four_engine.
- Rotorvox_C2A wikiPageWikiLink Fuselage.
- Rotorvox_C2A wikiPageWikiLink Germany.
- Rotorvox_C2A wikiPageWikiLink Hydraulic.
- Rotorvox_C2A wikiPageWikiLink Hydraulics.
- Rotorvox_C2A wikiPageWikiLink Landing_gear.
- Rotorvox_C2A wikiPageWikiLink Monocoque.
- Rotorvox_C2A wikiPageWikiLink Pre-rotation.
- Rotorvox_C2A wikiPageWikiLink Propeller_(aeronautics).
- Rotorvox_C2A wikiPageWikiLink Pusher_configuration.
- Rotorvox_C2A wikiPageWikiLink Rotax_914.
- Rotorvox_C2A wikiPageWikiLink Rotor.
- Rotorvox_C2A wikiPageWikiLink Rudder.
- Rotorvox_C2A wikiPageWikiLink Tailplane.
- Rotorvox_C2A wikiPageWikiLink Tandem.
- Rotorvox_C2A wikiPageWikiLink Ventral.
- Rotorvox_C2A wikiPageWikiLinkText "Rotorvox C2A".
- Rotorvox_C2A crew "Two".
- Rotorvox_C2A cruiseSpeedKmh "145".
- Rotorvox_C2A endurance "21600.0".
- Rotorvox_C2A eng1Kw "73".
- Rotorvox_C2A eng1Name Rotax_914.
- Rotorvox_C2A eng1Note "continuous".
- Rotorvox_C2A eng1Number "1".
- Rotorvox_C2A eng1Type "liquid-cooled flat-four".
- Rotorvox_C2A firstFlight "c.2009".
- Rotorvox_C2A grossWeightNote "useful load".
- Rotorvox_C2A hasPhotoCollection Rotorvox_C2A.
- Rotorvox_C2A heightM "2.85".
- Rotorvox_C2A lengthM "5.5".
- Rotorvox_C2A lengthNote "fuselage; including rotors".
- Rotorvox_C2A manufacturer "Rotorvox GGC GmbH".
- Rotorvox_C2A maxTakeoffWeightKg "560".
- Rotorvox_C2A nationalOrigin Germany.
- Rotorvox_C2A neverExceedSpeedKmh "164".
- Rotorvox_C2A primeUnits%3F_ "met".
- Rotorvox_C2A propBladeNumber "3".
- Rotorvox_C2A propDiaM "1.75".
- Rotorvox_C2A propName "Duc".
- Rotorvox_C2A rangeKm "600".
- Rotorvox_C2A ref "Jane's All the World's Aircraft 2015/16 p.279".
- Rotorvox_C2A rotDiaM "8.4".
- Rotorvox_C2A rotDiaNote "two aluminium blades, airfoil NACA 8H12".
- Rotorvox_C2A rotNumber "1".
- Rotorvox_C2A type "Two seat autogyro".
- Rotorvox_C2A widthM "2.21".
- Rotorvox_C2A widthNote "fuselage".
- Rotorvox_C2A wikiPageUsesTemplate Template:Aircraft_specs.
- Rotorvox_C2A wikiPageUsesTemplate Template:Convert.
- Rotorvox_C2A wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- Rotorvox_C2A wikiPageUsesTemplate Template:Reflist.
- Rotorvox_C2A subject Category:Autogyros.
- Rotorvox_C2A subject Category:German_aircraft_2000–2009.
- Rotorvox_C2A hypernym Seat.
- Rotorvox_C2A type Aircraft.
- Rotorvox_C2A type MeanOfTransportation.
- Rotorvox_C2A type Settlement.
- Rotorvox_C2A type Product.
- Rotorvox_C2A type DesignedArtifact.
- Rotorvox_C2A type Thing.
- Rotorvox_C2A type Q11436.
- Rotorvox_C2A comment "The Rotorvox C2A is a two seat, pusher configuration autogyro developed in Germany.".
- Rotorvox_C2A label "Rotorvox C2A".
- Rotorvox_C2A sameAs m.013f7m0x.
- Rotorvox_C2A wasDerivedFrom Rotorvox_C2A?oldid=668369914.
- Rotorvox_C2A isPrimaryTopicOf Rotorvox_C2A.