About: Raptor Aircraft Raptor

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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".

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft aircraft settlement
rdfs:label	Raptor Aircraft Raptor (en)
rdfs:comment	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". (en)
foaf:depiction
dcterms:subject	Homebuilt aircraft Single-engined pusher aircraft Canard aircraft Proposed aircraft of the United States
Wikipage page ID	49633298 (xsd:integer)
Wikipage revision ID	1098520070 (xsd:integer)
Link from a Wikipage to another Wikipage	Rutan VariEze Area rule Homebuilt aircraft Uber United States Valdosta Regional Airport Velocity SE Velocity XL Constant-speed propeller Medium.com Escrow General aviation Cirrus Aircraft Glassic SQ2000 Pressurization Berkut 360 Steve Wright Stagger-Ez Computer-aided design Synergy Aircraft Synergy Australia Australians Ball Ground, Georgia Ducted fan Homebuilt aircraft Single-engined pusher aircraft Aircraft Aircraft engine Rutan Defiant Prototype Pusher configuration Cozy III Audi Canard aircraft Proposed aircraft of the United States Landing gear Tricycle landing gear Diesel engine Cirrus SR22 Instrument flight rules Canard (aeronautics) YouTube Flap (aeronautics) Rutan Long-EZ Carbon fibre dbr:Raptor_Aircraft Wrist pin Box wing dbr:Raptor_Aircraft_Raptor_NG
Link from a Wikipage to an external page	http://www.raptor-aircraft.com/home.html https://medium.com/@RaptorAircraft
sameAs	Raptor Aircraft Raptor Raptor Aircraft Raptor
span ft	33 (xsd:integer)
span in	9 (xsd:integer)
stall speed kts	65 (xsd:integer)
wing area sqft	167 (xsd:integer)
wing loading lb/sqft	21.500000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:About dbt:Convert dbt:Infobox_aircraft_type dbt:Reflist dbt:Short_description dbt:Use_American_English dbt:Use_dmy_dates dbt:Aircraft_specs
thumbnail	wiki-commons:Special:FilePath/Raptor_Aircraft_Raptor_PR_photo_662.jpg?width=300
dbp:primeUnits%3F_	kts (en)
first flight	2020-10-10 (xsd:date)
national origin	United States Australia
capacity	three-four passengers (en)
crew	one (en)
designer	Peter Muller (en)
fuel capacity	usable (en)
height ft	10 (xsd:integer)
height in	0 (xsd:integer)
length ft	22 (xsd:integer)
manufacturer	Raptor Aircraft (en)
ref	the manufacturer (en)
status	Development ended (en)
type	Homebuilt aircraft
unit cost	130000.0 (usDollar)
has abstract	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". The prototype made its first substantive flight on 10 October 2020. During a ferry flight on 6 August 2021 the Raptor prototype crashed in a cornfield, suffering substantial damage. Subsequently, Muller announced that development of the Raptor would end and the company would move onto developing a derivative design, the . (en)
ceiling ft	27000 (xsd:integer)
climb rate ftmin	2000 (xsd:integer)

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