About: Grob GF 200

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An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.org associated with source document(s)
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http://dbpedia.org/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FGrob_GF_200&graph=http%3A%2F%2Fdbpedia.org&graph=http%3A%2F%2Fdbpedia.org

The Grob GF 200 was a business aircraft of unorthodox design developed in Germany during the 1990s.

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	Grob GF 200 (de) Grob GF 200 (en) Grob GF 200 (pt) 格罗伯GF 200 (zh)
rdfs:comment	Die Grob GF 200 war ein einmotoriges, viersitziges Geschäftsreiseflugzeug des deutschen Herstellers Burkhart Grob Luft- und Raumfahrt, bei dem ein Mittelmotor über eine Fernwelle einen Heckpropeller antrieb. (de) The Grob GF 200 was a business aircraft of unorthodox design developed in Germany during the 1990s. (en) O Grob GF 200 foi um projeto de avião executivo desenvolvido pela Grob Aircraft na Alemanha durante a década de 1980 e 1990. (pt) 格罗伯GF 200（英語：Grob GF 200）是一款由德國在1990年代研製的公務機，採用低單翼設計，設有可收縮起落架及機身外型高度流線型。飛機引擎裝在機身尾部，採用推进式螺旋桨，尾翼為T型尾翼設計，機翼設有翼尖小翼。機身下戶亦有一塊后机身下翼，飛機採用複合材料製造。格罗伯公司稱採用推进式螺旋桨與傳統螺旋桨的不同之與是，空氣流經機體上方的是層流。 GF 200最早源於1983年，當時格罗伯首席設計師希望能把複合材料應用到四座位的飛機上，但由於當時用複合材料製造的飛機較難取得認證，計劃被推遲至1988年。首架沒有加壓機艙的原型機在1991年11月26日首飛，在1992年柏林航空展首次公開亮相。初步飛行測試揭露飛機的引擎冷卻系統問題和噪音過高的問題。 (zh)
foaf:depiction
dcterms:subject	Grob aircraft 1990s German business aircraft Low-wing aircraft Single-engined pusher aircraft Aircraft first flown in 1991
Wikipage page ID	16917501 (xsd:integer)
Wikipage revision ID	1072191514 (xsd:integer)
Link from a Wikipage to another Wikipage	Grob aircraft 1990s German business aircraft Low-wing aircraft Single-engined pusher aircraft Flight International Grob Aircraft Aircraft first flown in 1991 LearAvia Lear Fan Cirrus VK-30 Lycoming O-540 Flat-six Berlin Air Show dbr:Hannover_Show
Link from a Wikipage to an external page	http://www.flightglobal.com/pdfarchive/view/1988/1988%20-%201271.html http://www.flightglobal.com/pdfarchive/view/1991/1991%20-%200702.html http://www.flightglobal.com/pdfarchive/view/1991/1991%20-%202858.html http://www.flightglobal.com/pdfarchive/view/1992/1992%20-%201611.html http://www.flightglobal.com/pdfarchive/view/1994/1994%20-%202808.html http://www.flightglobal.com/pdfarchive/view/1995/1995%20-%202614.html http://www.flightglobal.com/pdfarchive/view/1995/1995%20-%203319.html http://www.flightglobal.com/pdfarchive/view/1997/1997%20-%203165.html
sameAs	Grob GF 200 Grob GF 200 Grob GF 200 Grob GF 200 Grob GF 200 Grob GF 200
similar aircraft	Cirrus VK-30 LearAvia Lear Fan (en)
span m	11 (xsd:integer)
wing area sqm	12.530000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Cite_journal dbt:Commonscat dbt:Convert dbt:Refbegin dbt:Refend dbt:Reflist dbt:Grob_aircraft dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/Grob_GF200.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	1991-11-26 (xsd:date)
national origin	Germany (en)
capacity	3 (xsd:integer)
crew	One (en)
manufacturer	Grob Aircraft
ref	Jane's All The World's Aircraft 1992–93 (en)
type	Business aircraft (en)
has abstract	Die Grob GF 200 war ein einmotoriges, viersitziges Geschäftsreiseflugzeug des deutschen Herstellers Burkhart Grob Luft- und Raumfahrt, bei dem ein Mittelmotor über eine Fernwelle einen Heckpropeller antrieb. (de) The Grob GF 200 was a business aircraft of unorthodox design developed in Germany during the 1990s. (en) O Grob GF 200 foi um projeto de avião executivo desenvolvido pela Grob Aircraft na Alemanha durante a década de 1980 e 1990. (pt) 格罗伯GF 200（英語：Grob GF 200）是一款由德國在1990年代研製的公務機，採用低單翼設計，設有可收縮起落架及機身外型高度流線型。飛機引擎裝在機身尾部，採用推进式螺旋桨，尾翼為T型尾翼設計，機翼設有翼尖小翼。機身下戶亦有一塊后机身下翼，飛機採用複合材料製造。格罗伯公司稱採用推进式螺旋桨與傳統螺旋桨的不同之與是，空氣流經機體上方的是層流。 GF 200最早源於1983年，當時格罗伯首席設計師希望能把複合材料應用到四座位的飛機上，但由於當時用複合材料製造的飛機較難取得認證，計劃被推遲至1988年。首架沒有加壓機艙的原型機在1991年11月26日首飛，在1992年柏林航空展首次公開亮相。初步飛行測試揭露飛機的引擎冷卻系統問題和噪音過高的問題。 (zh)
ceiling m	7620 (xsd:integer)
climb rate ftmin	1220 (xsd:integer)
cruise speed kmh	445 (xsd:integer)
cruise speed note	(en)
eng1 hp	270 (xsd:integer)
eng1 name	Lycoming O-540
eng1 number	1 (xsd:integer)
eng1 type	air-cooled flat-six engine (en)
height m	3.200000 (xsd:double)
length m	8.500000 (xsd:double)
max takeoff weight kg	1450 (xsd:integer)
more performance	900.0 (second)
number built	1 (xsd:integer)

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