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- Bede_XBD-2 abstract "The Bede XBD-2 was an experimental short take-off and landing (STOL) aircraft, with several novel features such as structural use of glass-fibre and aluminium honeycomb, a suction boundary layer control (BLC) system and twin fuselage mounted engines driving a pusher configuration, shrouded single propeller. The sole example flew in the early 1960s in the USA.".
- Bede_XBD-2 manufacturer Bede_Aircraft.
- Bede_XBD-2 numberBuilt "1".
- Bede_XBD-2 origin United_States.
- Bede_XBD-2 type Experimental_aircraft.
- Bede_XBD-2 wikiPageExternalLink goe549.gif.
- Bede_XBD-2 wikiPageID "35742708".
- Bede_XBD-2 wikiPageRevisionID "606598702".
- Bede_XBD-2 airfoil "Göttingen 549".
- Bede_XBD-2 capacity "4".
- Bede_XBD-2 ceilingFt "21000".
- Bede_XBD-2 ceilingNote "service".
- Bede_XBD-2 climbRateFtmin "1050".
- Bede_XBD-2 crew "1".
- Bede_XBD-2 cruiseSpeedMph "179".
- Bede_XBD-2 cruiseSpeedNote "maximum at 65% power at 9,000ft".
- Bede_XBD-2 developedInto Bede_BD-3.
- Bede_XBD-2 eng1Hp "145".
- Bede_XBD-2 eng1Name "Continental O-300-A".
- Bede_XBD-2 eng1Number "2".
- Bede_XBD-2 eng1Type "6".
- Bede_XBD-2 firstFlight "1961-07-26".
- Bede_XBD-2 hasPhotoCollection Bede_XBD-2.
- Bede_XBD-2 heightM "3.78".
- Bede_XBD-2 lengthM "7.22".
- Bede_XBD-2 manufacturer Bede_Aircraft.
- Bede_XBD-2 maxSpeedMph "204".
- Bede_XBD-2 maxSpeedNote "at sea level".
- Bede_XBD-2 maxTakeoffWeightLb "3300".
- Bede_XBD-2 morePerformance "*Take-off run: less than 300 ft *Take-off distance to clear 50 ft : under 500 ft *Landing distance from 50 ft : under 500 ft".
- Bede_XBD-2 nationalOrigin United_States.
- Bede_XBD-2 numberBuilt "1".
- Bede_XBD-2 primeUnits%3F_ "imp".
- Bede_XBD-2 propName "Hartzell constant speed".
- Bede_XBD-2 ref "Jane's All the World's Aircraft 1962-63".
- Bede_XBD-2 spanM "11.42".
- Bede_XBD-2 stallSpeedMph "42".
- Bede_XBD-2 stallSpeedNote "with BLC. Without BLC 64 mph".
- Bede_XBD-2 type Experimental_aircraft.
- Bede_XBD-2 wingAreaSqm "13.94".
- Bede_XBD-2 subject Category:Bede_aircraft.
- Bede_XBD-2 subject Category:Ducted_fan-powered_aircraft.
- Bede_XBD-2 subject Category:Low-wing_aircraft.
- Bede_XBD-2 subject Category:Twin-engined_single-prop_pusher_aircraft.
- Bede_XBD-2 subject Category:United_States_experimental_aircraft_1960–1969.
- Bede_XBD-2 type Aircraft.
- Bede_XBD-2 type MeanOfTransportation.
- Bede_XBD-2 type Product.
- Bede_XBD-2 type DesignedArtifact.
- Bede_XBD-2 comment "The Bede XBD-2 was an experimental short take-off and landing (STOL) aircraft, with several novel features such as structural use of glass-fibre and aluminium honeycomb, a suction boundary layer control (BLC) system and twin fuselage mounted engines driving a pusher configuration, shrouded single propeller. The sole example flew in the early 1960s in the USA.".
- Bede_XBD-2 label "Bede XBD-2".
- Bede_XBD-2 label "Bede XBD-2".
- Bede_XBD-2 sameAs Bede_XBD-2.
- Bede_XBD-2 sameAs m.0jt0kt4.
- Bede_XBD-2 sameAs Q2893552.
- Bede_XBD-2 sameAs Q2893552.
- Bede_XBD-2 wasDerivedFrom Bede_XBD-2?oldid=606598702.
- Bede_XBD-2 isPrimaryTopicOf Bede_XBD-2.