The Raptor was a four to five-seat single-engined canard-wing homebuilt light aircraft, whose prototype was under development by of Ball Ground, Georgia, United States. The Raptor's tricycle landing gear was fully retractable, and the streamlined pressurized airframe was to be optimized for a fast cruising speed at high altitudes. The aircraft was intended to be supplied in kit form for amateur construction. The aircraft's designer is Australian Peter Muller, whose design goals were to provide a fast, spacious aircraft with IFR capability. Muller intended that the kit would be sold "at cost".
Property | Value |
---|---|
dbo:abstract |
|
dbo:manufacturer | |
dbo:origin | |
dbo:thumbnail | |
dbo:type | |
dbo:unitCost |
|
dbo:wikiPageExternalLink | |
dbo:wikiPageID |
|
dbo:wikiPageLength |
|
dbo:wikiPageRevisionID |
|
dbo:wikiPageWikiLink |
|
dbp:capacity |
|
dbp:ceilingFt |
|
dbp:climbRateFtmin |
|
dbp:climbRateNote |
|
dbp:crew |
|
dbp:cruiseSpeedKts |
|
dbp:cruiseSpeedNote |
|
dbp:designer |
|
dbp:emptyWeightLb |
|
dbp:eng1Hp |
|
dbp:eng1Name |
|
dbp:eng1Number |
|
dbp:firstFlight |
|
dbp:fuelCapacity |
|
dbp:grossWeightLb |
|
dbp:heightFt |
|
dbp:heightIn |
|
dbp:lengthFt |
|
dbp:lengthIn |
|
dbp:manufacturer |
|
dbp:nationalOrigin | |
dbp:numberBuilt |
|
dbp:primeUnits?_ |
|
dbp:rangeNmi |
|
dbp:ref |
|
dbp:spanFt |
|
dbp:spanIn |
|
dbp:stallSpeedKts |
|
dbp:status |
|
dbp:type | |
dbp:unitCost |
|
dbp:wikiPageUsesTemplate | |
dbp:wingAreaSqft |
|
dbp:wingLoadingLb/sqft |
|
dcterms:subject | |
gold:hypernym | |
rdf:type | |
rdfs:comment |
|
rdfs:label |
|
owl:sameAs | |
prov:wasDerivedFrom | |
foaf:depiction | |
foaf:isPrimaryTopicOf | |
is dbo:wikiPageDisambiguates of | |
is dbo:wikiPageWikiLink of | |
is foaf:primaryTopic of |