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- Leduc_0.21 abstract "The Leduc 0.21 was a research aircraft built in France in 1953 to refine the practicalities of ramjet propulsion. Initially proposed as the 0.20, it was essentially similar to its predecessor, the Leduc 0.10, but scaled up by around 30%, with tip tanks added to the wings. Again, it was not capable of take-off under its own power, and had to be carried aloft and released.Two examples were built and completed a very detailed flight test program from 1953 to 1956 to develop automated, operationally viable throttle controls for the ramjet. This included a total of 284 free flights. Designed for subsonic speeds only, the 0.21 reached a top speed of Mach 0.95.".
- Leduc_0.21 designer René_Leduc_(1898–1968).
- Leduc_0.21 manufacturer Breguet_Aviation.
- Leduc_0.21 numberBuilt "2".
- Leduc_0.21 wikiPageExternalLink stato-2.html.
- Leduc_0.21 wikiPageID "19368949".
- Leduc_0.21 wikiPageLength "4628".
- Leduc_0.21 wikiPageOutDegree "9".
- Leduc_0.21 wikiPageRevisionID "668327614".
- Leduc_0.21 wikiPageWikiLink Air_launch.
- Leduc_0.21 wikiPageWikiLink Breguet_Aviation.
- Leduc_0.21 wikiPageWikiLink Category:French_experimental_aircraft_1950–1959.
- Leduc_0.21 wikiPageWikiLink Category:Leduc_aircraft.
- Leduc_0.21 wikiPageWikiLink Drop_tank.
- Leduc_0.21 wikiPageWikiLink Leduc_0.10.
- Leduc_0.21 wikiPageWikiLink Ramjet.
- Leduc_0.21 wikiPageWikiLink René_Leduc_(1898–1968).
- Leduc_0.21 wikiPageWikiLink Speed_of_sound.
- Leduc_0.21 wikiPageWikiLinkText "0.21".
- Leduc_0.21 wikiPageWikiLinkText "Leduc 0.21".
- Leduc_0.21 crew "One".
- Leduc_0.21 designer René_Leduc_(1898–1968).
- Leduc_0.21 emptyWeightKg "3300".
- Leduc_0.21 emptyWeightLb "7260".
- Leduc_0.21 eng1Kn "63.7".
- Leduc_0.21 eng1Lbf "14300".
- Leduc_0.21 eng1Number "1".
- Leduc_0.21 eng1Type "Leduc ramjet".
- Leduc_0.21 firstFlight "1953-08-07".
- Leduc_0.21 grossWeightKg "6000".
- Leduc_0.21 grossWeightLb "13200".
- Leduc_0.21 lengthFt "41".
- Leduc_0.21 lengthIn "0".
- Leduc_0.21 lengthM "12.5".
- Leduc_0.21 manufacturer Breguet_Aviation.
- Leduc_0.21 maxSpeedKmh "900".
- Leduc_0.21 maxSpeedMph "560".
- Leduc_0.21 metOrEng%3F_ "met".
- Leduc_0.21 nationalOrigin "France".
- Leduc_0.21 numberBuilt "2".
- Leduc_0.21 spanFt "38".
- Leduc_0.21 spanIn "1".
- Leduc_0.21 spanM "11.6".
- Leduc_0.21 type "Research aircraft".
- Leduc_0.21 wikiPageUsesTemplate Template:Aerospecs.
- Leduc_0.21 wikiPageUsesTemplate Template:Aircontent.
- Leduc_0.21 wikiPageUsesTemplate Template:Cite_book.
- Leduc_0.21 wikiPageUsesTemplate Template:Commons_category.
- Leduc_0.21 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- Leduc_0.21 wikiPageUsesTemplate Template:Leduc_aircraft.
- Leduc_0.21 wingAreaSqft "237".
- Leduc_0.21 wingAreaSqm "22".
- Leduc_0.21 subject Category:French_experimental_aircraft_1950–1959.
- Leduc_0.21 subject Category:Leduc_aircraft.
- Leduc_0.21 hypernym Aircraft.
- Leduc_0.21 type Aircraft.
- Leduc_0.21 type MeanOfTransportation.
- Leduc_0.21 type Product.
- Leduc_0.21 type DesignedArtifact.
- Leduc_0.21 type Thing.
- Leduc_0.21 type Q11436.
- Leduc_0.21 comment "The Leduc 0.21 was a research aircraft built in France in 1953 to refine the practicalities of ramjet propulsion. Initially proposed as the 0.20, it was essentially similar to its predecessor, the Leduc 0.10, but scaled up by around 30%, with tip tanks added to the wings.".
- Leduc_0.21 label "Leduc 0.21".
- Leduc_0.21 sameAs Q6512772.
- Leduc_0.21 sameAs Leduc_0.21.
- Leduc_0.21 sameAs Leduc_0.21.
- Leduc_0.21 sameAs m.04n1204.
- Leduc_0.21 sameAs Leduc_0.21.
- Leduc_0.21 sameAs Q6512772.
- Leduc_0.21 wasDerivedFrom Leduc_0.21?oldid=668327614.
- Leduc_0.21 isPrimaryTopicOf Leduc_0.21.