About: Lancair Propjet

Facets (new session)
Description
Metadata
Settings
- Rule:
- Inverse Functional Properties:
- "Same As":

About: Lancair Propjet Goto Sponge NotDistinct Permalink

An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
QRcode icon

http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FLancair_Propjet&invfp=IFP_OFF&sas=SAME_AS_OFF

The Lancair Propjet is a four-seat, pressurized, composite aircraft powered by a 750-hp Walter M601E turboprop engine. The aircraft is based on Lancair's successful kit-plane, the Lancair IV. Like its piston-powered predecessor, the Propjet is noted for its performance, with a typical cruise speed of 325 knots at 24,000 feet and a climb performance of 4,000 feet per minute. Production of the aircraft kit was ended in 2012.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Abstraction100002137 yago:Category105838765 yago:Cognition100023271 yago:Concept105835747 yago:Content105809192 yago:Idea105833840 yago:Kind105839024 yago:PsychologicalFeature100023100 aircraft yago:Type105840188 umbel-rc:Model_airplane
rdfs:label	Lancair Propjet (de) Lancair Propjet (es) Lancair Propjet (en)
rdfs:comment	Der Lancair Propjet ist ein viersitziges Kitflugzeug der Firma Lancair. Er ist aus Verbundwerkstoffen hergestellt und wird von einem Turboproptriebwerk vom Typ Walter M601E mit einer Leistung von 750 PS (552 kW) angetrieben. Des Weiteren verfügt er über eine Druckkabine und ein einziehbares Bugradfahrwerk. Die Konstruktion basiert auf der Lancair IV. Das Flugzeug erreicht eine Reisegeschwindigkeit von 325 kn (602 km/h) auf einer Höhe von 24.000 ft (7.315 m) und eine Steiggeschwindigkeit von 4.000 Fuß pro Minute. Die Produktion des Lancair Propjet wurde 2012 eingestellt. (de) The Lancair Propjet is a four-seat, pressurized, composite aircraft powered by a 750-hp Walter M601E turboprop engine. The aircraft is based on Lancair's successful kit-plane, the Lancair IV. Like its piston-powered predecessor, the Propjet is noted for its performance, with a typical cruise speed of 325 knots at 24,000 feet and a climb performance of 4,000 feet per minute. Production of the aircraft kit was ended in 2012. (en) El Lancair Propjet es una aeronave presurizada de cuatro asientos o cuatriplaza impulsada por un motor turbohélice de 750 HP. El diseño de la aeronave se basa en el exitoso kit-plane Lancair IV. Al igual que su predecesor con motor de émbolo, el Lancair Propjet se caracteriza por su rendimiento, con una velocidad crucero típica de 325 nudos a 24 000 pies y un régimen de ascenso de 4000 pies por minuto. (es)
foaf:depiction
dcterms:subject	Lancair aircraft Low-wing aircraft Single-engined turboprop aircraft Homebuilt aircraft Single-engined tractor aircraft 2000s United States civil utility aircraft
Wikipage page ID	7959753 (xsd:integer)
Wikipage revision ID	997048246 (xsd:integer)
Link from a Wikipage to another Wikipage	Lancair aircraft Homebuilt aircraft Turboprop Gallon Composite material Low-wing aircraft Single-engined turboprop aircraft Homebuilt aircraft Single-engined tractor aircraft 2000s United States civil utility aircraft Lancair Lancair IV Cabin pressurization Walter M601 Piston engine Specific fuel consumption (thrust)
Link from a Wikipage to an external page	https://web.archive.org/web/20081216002700/http:/www.lancair.com/Main/iv_ivp.html
sameAs	Lancair Propjet Lancair Propjet Lancair Propjet Lancair Propjet Lancair Propjet Lancair Propjet Lancair Propjet Lancair Propjet
span ft	30 (xsd:integer)
span in	3 (xsd:integer)
span m	10.490000 (xsd:double)
stall speed kmh	120 (xsd:integer)
stall speed kts	64 (xsd:integer)
stall speed mph	74 (xsd:integer)
variants with their own articles	Lancair IV
wing area sqft	98 (xsd:integer)
wing area sqm	9.100000 (xsd:double)
wing loading kg/m	190.700000 (xsd:double)
wing loading lb/sqft	39 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Commons_category dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Lancair
thumbnail	wiki-commons:Special:FilePath/LancairIV-PPropjet02.jpg?width=300
dbp:primeUnits%3F_	kts (en)
capacity	3 (xsd:integer)
crew	one (en)
length ft	26 (xsd:integer)
manufacturer	Lancair
status	Production completed 2012 (en)
type	Homebuilt aircraft
has abstract	Der Lancair Propjet ist ein viersitziges Kitflugzeug der Firma Lancair. Er ist aus Verbundwerkstoffen hergestellt und wird von einem Turboproptriebwerk vom Typ Walter M601E mit einer Leistung von 750 PS (552 kW) angetrieben. Des Weiteren verfügt er über eine Druckkabine und ein einziehbares Bugradfahrwerk. Die Konstruktion basiert auf der Lancair IV. Das Flugzeug erreicht eine Reisegeschwindigkeit von 325 kn (602 km/h) auf einer Höhe von 24.000 ft (7.315 m) und eine Steiggeschwindigkeit von 4.000 Fuß pro Minute. Die Produktion des Lancair Propjet wurde 2012 eingestellt. (de) The Lancair Propjet is a four-seat, pressurized, composite aircraft powered by a 750-hp Walter M601E turboprop engine. The aircraft is based on Lancair's successful kit-plane, the Lancair IV. Like its piston-powered predecessor, the Propjet is noted for its performance, with a typical cruise speed of 325 knots at 24,000 feet and a climb performance of 4,000 feet per minute. Production of the aircraft kit was ended in 2012. (en) El Lancair Propjet es una aeronave presurizada de cuatro asientos o cuatriplaza impulsada por un motor turbohélice de 750 HP. El diseño de la aeronave se basa en el exitoso kit-plane Lancair IV. Al igual que su predecesor con motor de émbolo, el Lancair Propjet se caracteriza por su rendimiento, con una velocidad crucero típica de 325 nudos a 24 000 pies y un régimen de ascenso de 4000 pies por minuto. (es)
climb rate ftmin	7000 (xsd:integer)
climb rate note	; 4,000 ft/min (en)
cruise speed kmh	600 (xsd:integer)
cruise speed kts	325 (xsd:integer)
cruise speed mph	370 (xsd:integer)
cruise speed note	at 24,000 ft (en)
empty weight kg	1045 (xsd:integer)
empty weight lb	2300 (xsd:integer)
eng1 hp	750 (xsd:integer)
eng1 kw	559 (xsd:integer)
eng1 name	Walter M601E-11 turbine (en)
eng1 note	at sea level (en)
eng1 number	1 (xsd:integer)
length m	7.920000 (xsd:double)
max takeoff weight kg	1727 (xsd:integer)

Faceted Search & Find service v1.17_git139 as of Feb 29 2024

Alternative Linked Data Documents: ODE Content Formats:

RDF

ODATA

Microdata

About

OpenLink Virtuoso version 08.03.3330 as of Mar 19 2024, on Linux (x86_64-generic-linux-glibc212), Single-Server Edition (378 GB total memory, 67 GB memory in use)
Data on this page belongs to its respective rights holders.
Virtuoso Faceted Browser Copyright © 2009-2024 OpenLink Software