About: LAK Genesis 2

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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%2FLAK_Genesis_2

The Genesis 2 is a Standard Class competition glider that was designed by an American team led by Jerry Mercer. It was produced in Lithuania. It is notable in having almost no rear fuselage. However it is not tailless, because it has a small, all-moving tailplane on top of the vertical stabilizer. The tailplane is mainly a trimmer, rather than for longitudinal stability.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:WikicatSailplanes yago:Aircraft102686568 yago:Artifact100021939 yago:Conveyance103100490 yago:Craft103125870 yago:Glider103439814 yago:Heavier-than-airCraft103510583 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 aircraft yago:Vehicle104524313 yago:Whole100003553 umbel-rc:Model_airplane
rdfs:label	Sportinė Aviacija Genesis 2 (de) LAK Genesis 2 (en)
rdfs:comment	Die Genesis 2 ist ein einsitziges Segelflugzeug der FAI-Standardklasse des litauischen Herstellers . Besonders auffällig an dem Flugzeug ist das stark verkürzte Heck, wodurch die Auslegung den Eindruck eines schwanzlosen Flugzeugs erweckt. (de) The Genesis 2 is a Standard Class competition glider that was designed by an American team led by Jerry Mercer. It was produced in Lithuania. It is notable in having almost no rear fuselage. However it is not tailless, because it has a small, all-moving tailplane on top of the vertical stabilizer. The tailplane is mainly a trimmer, rather than for longitudinal stability. (en)
foaf:depiction
dcterms:subject	LAK aircraft Marske aircraft Aircraft first flown in 1994 T-tail aircraft Glider aircraft Mid-wing aircraft
Wikipage page ID	22322463 (xsd:integer)
Wikipage revision ID	1108167716 (xsd:integer)
Link from a Wikipage to another Wikipage	Lithuania LAK aircraft Pultrusion Marske aircraft FAI Standard Class Trim (aircraft) Fuselage Aircraft first flown in 1994 T-tail aircraft Glider (sailplane) John Roncz Glider aircraft Mid-wing aircraft Tailplane Tailless aircraft Vertical stabilizer Washout (aviation) dbr:Litovskaya_Aviatsionnaya_Konstruktsiya dbr:Sportinė_Aviacija
Link from a Wikipage to an external page	https://web.archive.org/web/20120829145817/http:/www.sailplanedirectory.com/PlaneDetails.cfm%3FplaneID=119%7Carchivedate=29 http://www.sailplanedirectory.com/PlaneDetails.cfm%3FplaneID=119%7Ctitle=Genesis http://www.lak.lt
sameAs	LAK Genesis 2 LAK Genesis 2 LAK Genesis 2 LAK Genesis 2 LAK Genesis 2
sink rate ftmin	114 (xsd:integer)
sink rate ms	0.580000 (xsd:double)
span ft	49 (xsd:integer)
span in	3 (xsd:integer)
span m	15 (xsd:integer)
stall speed kmh	75 (xsd:integer)
stall speed mph	46.600000 (xsd:double)
wing area sqft	121 (xsd:integer)
wing area sqm	11.250000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:LAK_aircraft dbt:Marske_Aircraft dbt:Cite_book dbt:Cite_web dbt:Commons_category dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs
thumbnail	wiki-commons:Special:FilePath/KN_Genesis2_1995.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	1994 (xsd:integer)
national origin	Lithuania (en)
crew	one (en)
designer	Jim Marske and John Roncz (en)
height ft	7 (xsd:integer)
height in	3 (xsd:integer)
length ft	15 (xsd:integer)
manufacturer	Sportinė Aviacija (en)
ref	0001-08-14 (xsd:gMonthDay)
type	Standard Class sailplane (en)
has abstract	Die Genesis 2 ist ein einsitziges Segelflugzeug der FAI-Standardklasse des litauischen Herstellers . Besonders auffällig an dem Flugzeug ist das stark verkürzte Heck, wodurch die Auslegung den Eindruck eines schwanzlosen Flugzeugs erweckt. (de) The Genesis 2 is a Standard Class competition glider that was designed by an American team led by Jerry Mercer. It was produced in Lithuania. It is notable in having almost no rear fuselage. However it is not tailless, because it has a small, all-moving tailplane on top of the vertical stabilizer. The tailplane is mainly a trimmer, rather than for longitudinal stability. (en)
aspect ratio	20.200000 (xsd:double)
empty weight kg	240 (xsd:integer)
empty weight lb	530 (xsd:integer)
g limits	+5.55/-3.55 (en)
glide ratio	44 (xsd:integer)
gross weight kg	525 (xsd:integer)
gross weight lb	1157 (xsd:integer)
height m	2.210000 (xsd:double)
length in	10 (xsd:integer)
length m	4.828000 (xsd:double)

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