About: Rand Robinson KR-1

An Entity of Type: Homebuilt aircraft, from Named Graph: http://dbpedia.org, within Data Space: dbpedia.org

The Rand Robinson KR-1 is a single-seat, single-engine sport aircraft designed in the United States in the early 1970s and marketed for homebuilding. A two-seat version is marketed as the KR-2. It is a low-wing cantilever monoplane of conventional design with an enclosed cockpit and tailwheel undercarriage. As originally designed, the main undercarriage units of the KR-1 and basic KR-2 were manually retractable, folding backwards into the wings, while the KR-2T tandem-seat version had fixed tricycle undercarriage. However, some builders choose fixed tailwheel or even fixed tricycle undercarriage for KR-1s and KR-2s.

Property	Value
dbo:abstract	The Rand Robinson KR-1 is a single-seat, single-engine sport aircraft designed in the United States in the early 1970s and marketed for homebuilding. A two-seat version is marketed as the KR-2. It is a low-wing cantilever monoplane of conventional design with an enclosed cockpit and tailwheel undercarriage. As originally designed, the main undercarriage units of the KR-1 and basic KR-2 were manually retractable, folding backwards into the wings, while the KR-2T tandem-seat version had fixed tricycle undercarriage. However, some builders choose fixed tailwheel or even fixed tricycle undercarriage for KR-1s and KR-2s. Kits for the KR-1, KR-2 and KR-2S are supplied by of Mission Viejo, California/Corona, California, United States. (en)
dbo:manufacturer	dbr:NVAero
dbo:origin	dbr:United_States
dbo:thumbnail	wiki-commons:Special:FilePath/Chris_Gardiner's_1999_Rand_KR-2S_C-GKRZ_photo_1.jpg?width=300
dbo:type	dbr:Homebuilt_aircraft
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dbp:ceilingFt	15000 (xsd:integer)
dbp:climbRateFtmin	800 (xsd:integer)
dbp:cruiseSpeedMph	150 (xsd:integer)
dbp:designer	Kenneth Rand (en)
dbp:emptyWeightLb	480 (xsd:integer)
dbp:eng1Hp	80 (xsd:integer)
dbp:eng1Name	dbr:Volkswagen_air-cooled_engine
dbp:eng1Number	1 (xsd:integer)
dbp:eng1Type	flat four cylinder (en)
dbp:firstFlight	February 1972 (en)
dbp:grossWeightLb	900 (xsd:integer)
dbp:lengthFt	14 (xsd:integer)
dbp:lengthIn	6 (xsd:integer)
dbp:manufacturer	dbr:NVAero
dbp:nationalOrigin	United States (en)
dbp:primeUnits?_	imp (en)
dbp:rangeMiles	1300 (xsd:integer)
dbp:rangeNote	with of fuel (en)
dbp:ref	nVAero (en)
dbp:spanFt	20 (xsd:integer)
dbp:spanIn	8 (xsd:integer)
dbp:stallSpeedMph	52 (xsd:integer)
dbp:status	In production (en)
dbp:type	dbr:Homebuilt_aircraft
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dbp:wingAreaSqft	80 (xsd:integer)
dbp:wingLoadingLb/sqft	14.400000 (xsd:double)
dbp:wingLoadingNote	at 1150 lbs gross weight (en)
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rdfs:comment	The Rand Robinson KR-1 is a single-seat, single-engine sport aircraft designed in the United States in the early 1970s and marketed for homebuilding. A two-seat version is marketed as the KR-2. It is a low-wing cantilever monoplane of conventional design with an enclosed cockpit and tailwheel undercarriage. As originally designed, the main undercarriage units of the KR-1 and basic KR-2 were manually retractable, folding backwards into the wings, while the KR-2T tandem-seat version had fixed tricycle undercarriage. However, some builders choose fixed tailwheel or even fixed tricycle undercarriage for KR-1s and KR-2s. (en)
rdfs:label	Rand Robinson KR-1 (en)
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