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- Grob_GF_200 abstract "The Grob GF 200 was a business aircraft of unorthodox design developed in Germany during the 1990s. It was a low-wing cantilever monoplane with retractable tricycle undercarriage and a highly streamlined fuselage. The engine was mounted within the fuselage, to the rear of the passenger cabin, and drove the pusher propeller via a driveshaft. The GF 200 has a T-tail, but also a large ventral fin beneath the fuselage. Like other Grob designs, construction throughout was of composite materials, in the case of this particular aircraft, including the driveshaft.Development commenced in 1983 but was postponed due to concerns about achieving certification for the composite design. However, with financial support from the German government, development commenced in earnest by the end of the decade. The project officially launched at the Hannover Show in May 1988, at which a mockup of the design was displayed and a hope expressed to have the aircraft flying within two years. As it transpired, the prototype was rolled out in March 1991, in the hope of a first flight by May, and which finally took place on 26 November.The aircraft made its first public appearance at the Berlin Air Show in 1992. Initial flight tests revealed problems with engine cooling and excessive noise. The former concern was addressed by a redesign of the engine air intakes.The prototype was intended as a test aircraft and technology demonstrator, and lacked many of the refinements that would have been incorporated into a production aircraft, including cabin presurisation, de-icing equipment, and even a complete cabin interior. When Grob was unable to find financial backing to take the design further, the company embarked on the construction of a more "true-to-life" prototype in 1997, the GF 250, in the belief that this would prove more attractive to potential business partners.Further planned developments included the turboshaft-powered GF 300, and the GF 350 with twin turboshaft engines driving a common propeller.".
- Grob_GF_200 manufacturer Grob_Aircraft.
- Grob_GF_200 numberBuilt "1".
- Grob_GF_200 wikiPageExternalLink 1988%20-%201271.html.
- Grob_GF_200 wikiPageExternalLink 1991%20-%200702.html.
- Grob_GF_200 wikiPageExternalLink 1991%20-%202858.html.
- Grob_GF_200 wikiPageExternalLink 1992%20-%201611.html.
- Grob_GF_200 wikiPageExternalLink 1994%20-%202808.html.
- Grob_GF_200 wikiPageExternalLink 1995%20-%202614.html.
- Grob_GF_200 wikiPageExternalLink 1995%20-%203319.html.
- Grob_GF_200 wikiPageExternalLink 1997%20-%203165.html.
- Grob_GF_200 wikiPageExternalLink www.grob-aircraft.com.
- Grob_GF_200 wikiPageID "16917501".
- Grob_GF_200 wikiPageLength "7679".
- Grob_GF_200 wikiPageOutDegree "16".
- Grob_GF_200 wikiPageRevisionID "683744055".
- Grob_GF_200 wikiPageWikiLink Berlin_Air_Show.
- Grob_GF_200 wikiPageWikiLink Category:German_business_aircraft_1990–1999.
- Grob_GF_200 wikiPageWikiLink Category:Grob_aircraft.
- Grob_GF_200 wikiPageWikiLink Category:Pusher_aircraft.
- Grob_GF_200 wikiPageWikiLink Category:Tail-propeller_aircraft.
- Grob_GF_200 wikiPageWikiLink Continental_IO-550.
- Grob_GF_200 wikiPageWikiLink Flight_International.
- Grob_GF_200 wikiPageWikiLink Grob_Aircraft.
- Grob_GF_200 wikiPageWikiLink Hannover_Show.
- Grob_GF_200 wikiPageWikiLink ILA_Berlin_Air_Show.
- Grob_GF_200 wikiPageWikiLink Teledyne_Continental_TSIOL-550.
- Grob_GF_200 wikiPageWikiLinkText "Grob GF 200".
- Grob_GF_200 capacity "4".
- Grob_GF_200 climbRateFtmin "1220".
- Grob_GF_200 climbRateMs "6.2".
- Grob_GF_200 crew "One pilot".
- Grob_GF_200 cruiseSpeedKmh "370".
- Grob_GF_200 cruiseSpeedMph "230".
- Grob_GF_200 eng1Hp "310".
- Grob_GF_200 eng1Kw "230".
- Grob_GF_200 eng1Number "1".
- Grob_GF_200 eng1Type Continental_IO-550.
- Grob_GF_200 eng1Type Teledyne_Continental_TSIOL-550.
- Grob_GF_200 firstFlight "1991-11-26".
- Grob_GF_200 grossWeightKg "1600".
- Grob_GF_200 grossWeightLb "3527".
- Grob_GF_200 hasPhotoCollection Grob_GF_200.
- Grob_GF_200 heightFt "11".
- Grob_GF_200 heightIn "3".
- Grob_GF_200 heightM "3.42".
- Grob_GF_200 lengthFt "28".
- Grob_GF_200 lengthIn "6".
- Grob_GF_200 lengthM "8.7".
- Grob_GF_200 manufacturer Grob_Aircraft.
- Grob_GF_200 metOrEng%3F_ "met".
- Grob_GF_200 nationalOrigin "Germany".
- Grob_GF_200 numberBuilt "1".
- Grob_GF_200 rangeKm "1850".
- Grob_GF_200 rangeMiles "1160".
- Grob_GF_200 spanFt "36".
- Grob_GF_200 spanIn "1".
- Grob_GF_200 spanM "11".
- Grob_GF_200 type "Business aircraft".
- Grob_GF_200 wikiPageUsesTemplate Template:Aerospecs.
- Grob_GF_200 wikiPageUsesTemplate Template:Aircontent.
- Grob_GF_200 wikiPageUsesTemplate Template:Cite_book.
- Grob_GF_200 wikiPageUsesTemplate Template:Cite_journal.
- Grob_GF_200 wikiPageUsesTemplate Template:Commons_category.
- Grob_GF_200 wikiPageUsesTemplate Template:Grob_aircraft.
- Grob_GF_200 wikiPageUsesTemplate Template:Infobox_Aircraft_Type.
- Grob_GF_200 wingAreaSqft "135".
- Grob_GF_200 wingAreaSqm "12.5".
- Grob_GF_200 subject Category:German_business_aircraft_1990–1999.
- Grob_GF_200 subject Category:Grob_aircraft.
- Grob_GF_200 subject Category:Pusher_aircraft.
- Grob_GF_200 subject Category:Tail-propeller_aircraft.
- Grob_GF_200 hypernym Aircraft.
- Grob_GF_200 type Aircraft.
- Grob_GF_200 type MeanOfTransportation.
- Grob_GF_200 type Product.
- Grob_GF_200 type DesignedArtifact.
- Grob_GF_200 type Thing.
- Grob_GF_200 type Q11436.
- Grob_GF_200 comment "The Grob GF 200 was a business aircraft of unorthodox design developed in Germany during the 1990s. It was a low-wing cantilever monoplane with retractable tricycle undercarriage and a highly streamlined fuselage. The engine was mounted within the fuselage, to the rear of the passenger cabin, and drove the pusher propeller via a driveshaft. The GF 200 has a T-tail, but also a large ventral fin beneath the fuselage.".
- Grob_GF_200 label "Grob GF 200".
- Grob_GF_200 sameAs m.04122_3.
- Grob_GF_200 sameAs Q5609891.
- Grob_GF_200 sameAs Q5609891.
- Grob_GF_200 wasDerivedFrom Grob_GF_200?oldid=683744055.
- Grob_GF_200 isPrimaryTopicOf Grob_GF_200.