About: Caspar C 17

Property	Value
dbo:abstract	The Caspar C 17 was a mid-1920s German, low power, two seat ultralight aircraft with a cantilever wing of unusually high aspect ratio, flexibly attached to the fuselage to moderate gust effects. (en) Le Caspar C 17 est un avion ultra-léger biplace, de faible puissance, construit en Allemagne au milieu des années 1920. Son aile en porte-à-faux présentait une finesse exceptionnellement élevée. Elle était reliée au fuselage de façon flexible, afin d'atténuer les effets des rafales de vent. (fr)
dbo:origin	dbr:Germany
dbo:thumbnail	wiki-commons:Special:FilePath/Caspar_C_17_NACA-TM-370.jpg?width=300
dbo:type	dbr:Ultralight
dbo:wikiPageID	53761380 (xsd:integer)
dbo:wikiPageLength	7673 (xsd:nonNegativeInteger)
dbo:wikiPageRevisionID	1123729293 (xsd:integer)
dbo:wikiPageWikiLink	dbr:Elevator_(aeronautics) dbr:Monoplane dbr:Ultralight dbr:Germany dbr:Low_wing dbr:Empennage dbr:Plywood dbr:Spar_(aeronautics) dbr:Stringer_(aircraft) dbr:Strut dbr:Tandem dbc:Low-wing_aircraft dbr:Fuselage dbr:Leading_edge dbr:Ailerons dbr:Aircraft_fairing dbr:Angle_of_attack dbr:Glider_(aircraft) dbr:Trailing_edge dbr:ABC_Scorpion dbc:Aircraft_first_flown_in_1924 dbc:1920s_German_sport_aircraft dbr:Landing_gear dbr:Cockpit dbr:Aspect_ratio_(aeronautics) dbr:Induced_drag dbr:Cantilever dbc:Caspar_aircraft dbr:Rudder dbr:Ultralight_aircraft dbr:Flat_twin dbr:All-moving_tailplane dbr:File:Caspar_C.17_3-view_NACA-TM-301.jpg dbr:Knoller-Betz
dbp:airfoil	Göttingen 348 (en)
dbp:aspectRatio	9.200000 (xsd:double)
dbp:ceilingM	3500 (xsd:integer)
dbp:crew	Two (en)
dbp:designer	Ernst Ritter von Loessel (en)
dbp:emptyWeightKg	145 (xsd:integer)
dbp:endurance	-9000.0
dbp:eng1Hp	30 (xsd:integer)
dbp:eng1Name	dbr:ABC_Scorpion
dbp:eng1Note	maximum, at 3,200 rpm (en)
dbp:eng1Number	1 (xsd:integer)
dbp:eng1Type	air-cooled flat twin (en)
dbp:firstFlight	1924 (xsd:integer)
dbp:grossWeightKg	325 (xsd:integer)
dbp:heightM	1.900000 (xsd:double)
dbp:lengthM	5.100000 (xsd:double)
dbp:manufacturer	Caspar-Travermünde Flugzeugerke (en)
dbp:maxSpeedKmh	110 (xsd:integer)
dbp:morePerformance	Take-off distance: Landing speed: (en)
dbp:nationalOrigin	dbr:Germany
dbp:primeUnits?_	met (en)
dbp:propBladeNumber	2 (xsd:integer)
dbp:propDiaM	1.200000 (xsd:double)
dbp:propName	Bork (en)
dbp:rangeKm	200 (xsd:integer)
dbp:ref	Les Ailes, January 1925 (en)
dbp:spanM	12 (xsd:integer)
dbp:timeToAltitude	720.0
dbp:type	Two seat ultralight (en)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Cvt dbt:Reflist dbt:Caspar_aircraft dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
dbp:wingAreaSqm	15.600000 (xsd:double)
dcterms:subject	dbc:Low-wing_aircraft dbc:Aircraft_first_flown_in_1924 dbc:1920s_German_sport_aircraft dbc:Caspar_aircraft
rdf:type	owl:Thing schema:Product dbo:MeanOfTransportation wikidata:Q11436 dbo:Aircraft
rdfs:comment	The Caspar C 17 was a mid-1920s German, low power, two seat ultralight aircraft with a cantilever wing of unusually high aspect ratio, flexibly attached to the fuselage to moderate gust effects. (en) Le Caspar C 17 est un avion ultra-léger biplace, de faible puissance, construit en Allemagne au milieu des années 1920. Son aile en porte-à-faux présentait une finesse exceptionnellement élevée. Elle était reliée au fuselage de façon flexible, afin d'atténuer les effets des rafales de vent. (fr)
rdfs:label	Caspar C 17 (en) Caspar C 17 (fr)
owl:sameAs	wikidata:Caspar C 17 dbpedia-fr:Caspar C 17 https://global.dbpedia.org/id/2qgPz
prov:wasDerivedFrom	wikipedia-en:Caspar_C_17?oldid=1123729293&ns=0
foaf:depiction	wiki-commons:Special:FilePath/Caspar_C.17_3-view_NACA-TM-301.jpg wiki-commons:Special:FilePath/Caspar_C_17_NACA-TM-370.jpg
foaf:isPrimaryTopicOf	wikipedia-en:Caspar_C_17
is dbo:wikiPageWikiLink of	dbr:List_of_aircraft_(C–Cc)
is foaf:primaryTopic of	wikipedia-en:Caspar_C_17