The Hurel-Dubois Miles HDM.105 was a transport aircraft fitted with very high aspect ratio wings for research purposes, building on research carried out with the Hurel-Dubois HD.10, and a stepping point to the planned production HDM.106 Caravan. The HDM.105/HDM.106 provided the starting point for the design of the Short SC.7 Skyvan.
| Attributes | Values |
|---|
| rdf:type
| |
| rdfs:label
| - Hurel-Dubois Miles HDM.105 (de)
- Hurel-Dubois Miles HDM.105 (it)
- Hurel-Dubois Miles HDM.105 (en)
|
| rdfs:comment
| - Die Hurel-Dubois Miles HDM.105 war ein Transportflugzeug mit sehr stark gestreckten Tragflächen zu Forschungszwecken, dessen Entwicklung auf Erkenntnisse aus der Entwicklung der aufbaute und ein wichtiger Schritt zum geplanten Bau der HDM.106 Caravan darstellte. Die Entwicklung der HDM.105/HDM.106 bildete den Ausgangspunkt für die Konstruktion der Short Skyvan. (de)
- The Hurel-Dubois Miles HDM.105 was a transport aircraft fitted with very high aspect ratio wings for research purposes, building on research carried out with the Hurel-Dubois HD.10, and a stepping point to the planned production HDM.106 Caravan. The HDM.105/HDM.106 provided the starting point for the design of the Short SC.7 Skyvan. (en)
- L'Hurel-Dubois Miles HDM.105 era un aereo da trasporto bimotore e monoplano ad ala alta progettato dall'ingegnere aeronautico francese negli anni cinquanta e costruito dall'azienda aeronautica britannica . Caratterizzato da un'ala ad elevatissimo allungamento alare, con piano alare rinforzato da robuste aste di controvento, il prototipo venne realizzato per scopi di ricerca, basandosi sulle ricerche condotte con l', e fu un punto di partenza per quello che doveva diventare il modello di produzione in serie, HDM.106 Caravan, produzione mai avviata. (it)
|
| dcterms:subject
| |
| Wikipage page ID
| |
| Wikipage revision ID
| |
| Link from a Wikipage to another Wikipage
| |
| sameAs
| |
| span ft
| |
| span in
| |
| wing area note
| - wings only, including struts (en)
|
| wing area sqft
| |
| dbp:wikiPageUsesTemplate
| |
| dbp:primeUnits%3F_
| |
| first flight
| |
| national origin
| |
| capacity
| - up to 9 passengers or freight (en)
|
| crew
| |
| designer
| |
| fuel capacity
| - in left and right vertical undercarriage strut fairings (en)
|
| height ft
| |
| height in
| |
| length ft
| |
| manufacturer
| |
| ref
| - Flight : Foretaste of the Caravan - HDM.105 handling HDM.106 prospects, Jane's All the World's Aircraft 1958-59, Miles aircraft since 1925 (en)
|
| type
| - Very high aspect ratio wing research (en)
|
| has abstract
| - Die Hurel-Dubois Miles HDM.105 war ein Transportflugzeug mit sehr stark gestreckten Tragflächen zu Forschungszwecken, dessen Entwicklung auf Erkenntnisse aus der Entwicklung der aufbaute und ein wichtiger Schritt zum geplanten Bau der HDM.106 Caravan darstellte. Die Entwicklung der HDM.105/HDM.106 bildete den Ausgangspunkt für die Konstruktion der Short Skyvan. (de)
- The Hurel-Dubois Miles HDM.105 was a transport aircraft fitted with very high aspect ratio wings for research purposes, building on research carried out with the Hurel-Dubois HD.10, and a stepping point to the planned production HDM.106 Caravan. The HDM.105/HDM.106 provided the starting point for the design of the Short SC.7 Skyvan. (en)
- L'Hurel-Dubois Miles HDM.105 era un aereo da trasporto bimotore e monoplano ad ala alta progettato dall'ingegnere aeronautico francese negli anni cinquanta e costruito dall'azienda aeronautica britannica . Caratterizzato da un'ala ad elevatissimo allungamento alare, con piano alare rinforzato da robuste aste di controvento, il prototipo venne realizzato per scopi di ricerca, basandosi sulle ricerche condotte con l', e fu un punto di partenza per quello che doveva diventare il modello di produzione in serie, HDM.106 Caravan, produzione mai avviata. (it)
|
| airfoil
| - root: NACA 634-420; tip: NACA 631-412 (en)
|
| aspect ratio
| |
| ceiling ft
| |
| climb rate ftmin
| |
| climb rate note
| - *Rate of climb on one engine: (en)
|
| cruise speed mph
| |
| cruise speed note
| |
| developed from
| |
| empty weight lb
| |
| eng1 hp
| |
| eng1 name
| |
| eng1 number
| |
| eng1 type
| |
| gross weight lb
| |
| length in
| |
| max speed kmh
| |
| max speed note
| |
| more performance
| - *Take-off run: minimum
*Take-off distance to : (en)
|
| number built
| |
| prop blade number
| |
| prop name
| - Fairey fixed-pitch propellers (en)
|
| prov:wasDerivedFrom
| |
| page length (characters) of wiki page
| |
| number built
| |
| designer
| |
| manufacturer
| |
| origin
| |
| predecessor
| |
| foaf:isPrimaryTopicOf
| |
![[RDF Data]](/fct/images/sw-rdf-blue.png)
![[cxml]](/fct/images/cxml_doc.png)
![[csv]](/fct/images/csv_doc.png)
![[text]](/fct/images/ntriples_doc.png)
![[turtle]](/fct/images/n3turtle_doc.png)
![[ld+json]](/fct/images/jsonld_doc.png)
![[rdf+json]](/fct/images/json_doc.png)
![[rdf+xml]](/fct/images/xml_doc.png)
![[atom+xml]](/fct/images/atom_doc.png)
![[html]](/fct/images/html_doc.png)