About: Rand Robinson KR-1

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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.

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
rdfs:label	Rand Robinson KR-1 (en)
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)
foaf:homepage	https://web.archive.org/web/20210506074222/http:/www.nvaero.com/
foaf:depiction
dcterms:subject	Aircraft first flown in 1972 Low-wing aircraft Homebuilt aircraft Single-engined tractor aircraft 1970s United States sport aircraft
Wikipage page ID	21245010 (xsd:integer)
Wikipage revision ID	1097754110 (xsd:integer)
Link from a Wikipage to another Wikipage	Queensland Air Museum Homebuilt aircraft United States Volkswagen air-cooled engine Corona, California Mission Viejo, California Empennage Aircraft first flown in 1972 Low-wing aircraft Wings Over the Rockies Air and Space Museum Airfoil Homebuilt aircraft Single-engined tractor aircraft EAA AirVenture Museum 1970s United States sport aircraft Jabiru 2200 Jabiru 3300 dbr:NVAero Tandem-seat
Link from a Wikipage to an external page	https://archive.org/details/janesallworldsai0000unse http://nv-aero.com/ http://www.nvaero.com/ http://www.airventuremuseum.org/collection/aircraft/Rand%20Robinson%20KR-1.asp https://web.archive.org/web/20210506074222/http:/www.nvaero.com/
sameAs	Rand Robinson KR-1 Rand Robinson KR-1 Rand Robinson KR-1 Rand Robinson KR-1
span ft	20 (xsd:integer)
span in	8 (xsd:integer)
stall speed mph	52 (xsd:integer)
wing area sqft	80 (xsd:integer)
wing loading lb/sqft	14.400000 (xsd:double)
wing loading note	at 1150 lbs gross weight (en)
dbp:wikiPageUsesTemplate	dbt:Authority_control dbt:Cite_book dbt:Cite_journal dbt:Cite_web dbt:Commons_category dbt:Convert dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:Rand_aircraft
thumbnail	wiki-commons:Special:FilePath/Chris_Gardiner's_1999_Rand_KR-2S_C-GKRZ_photo_1.jpg?width=300
dbp:primeUnits%3F_	imp (en)
first flight	February 1972 (en)
national origin	United States (en)
designer	Kenneth Rand (en)
length ft	14 (xsd:integer)
manufacturer	dbr:NVAero
ref	nVAero (en)
status	In production (en)
type	Homebuilt aircraft
has 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)
ceiling ft	15000 (xsd:integer)
climb rate ftmin	800 (xsd:integer)
cruise speed mph	150 (xsd:integer)
empty weight lb	480 (xsd:integer)
eng1 hp	80 (xsd:integer)
eng1 name	Volkswagen air-cooled engine
eng1 number	1 (xsd:integer)
eng1 type	flat four cylinder (en)
gross weight lb	900 (xsd:integer)
length in	6 (xsd:integer)
range miles	1300 (xsd:integer)
range note	with of fuel (en)
gold:hypernym	Aircraft
prov:wasDerivedFrom	wikipedia-en:Rand_Robinson_KR-1?oldid=1097754110&ns=0
page length (characters) of wiki page	11071 (xsd:nonNegativeInteger)

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