About: CARMAM 15-38

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An Entity of Type : umbel-rc:Model_airplane, within Data Space : dbpedia.demo.openlinksw.com associated with source document(s)
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http://dbpedia.demo.openlinksw.com/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FCARMAM_15-38&invfp=IFP_OFF&sas=SAME_AS_OFF

The CARMAM 15-38 was a French sailplane built in the late 1970s. It utilised the wing design of the CARMAM Aiglon but had an all-new fuselage. Like the Aiglon, this was of fibreglass construction throughout. The 15-38 was easily distinguished from its predecessor by a more streamlined nose and a T-tail.

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	CARMAM 15-38 (en)
rdfs:comment	The CARMAM 15-38 was a French sailplane built in the late 1970s. It utilised the wing design of the CARMAM Aiglon but had an all-new fuselage. Like the Aiglon, this was of fibreglass construction throughout. The 15-38 was easily distinguished from its predecessor by a more streamlined nose and a T-tail. (en)
dcterms:subject	T-tail aircraft Aircraft first flown in 1979 Glider aircraft 1970s French sailplanes
Wikipage page ID	14604980 (xsd:integer)
Wikipage revision ID	1123003157 (xsd:integer)
Link from a Wikipage to another Wikipage	1979 in aviation T-tail aircraft Aircraft first flown in 1979 Glider aircraft CARMAM CARMAM Aiglon 1970s French sailplanes
sameAs	CARMAM 15-38 CARMAM 15-38 CARMAM 15-38 CARMAM 15-38
sink rate ftmin	118 (xsd:integer)
sink rate ms	0.600000 (xsd:double)
span ft	49 (xsd:integer)
span in	3 (xsd:integer)
span m	15 (xsd:integer)
wing area sqft	118 (xsd:integer)
wing area sqm	11 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Cite_book dbt:Short_description dbt:Aircontent dbt:Aircraft_specs dbt:Infobox_Aircraft_Type dbt:Aero-1970s-stub
dbp:primeUnits%3F_	met (en)
first flight	1979-06-17 (xsd:date)
crew	One pilot (en)
height ft	4 (xsd:integer)
height in	9 (xsd:integer)
length ft	22 (xsd:integer)
manufacturer	CARMAM
type	Standard Class sailplane (en)
has abstract	The CARMAM 15-38 was a French sailplane built in the late 1970s. It utilised the wing design of the CARMAM Aiglon but had an all-new fuselage. Like the Aiglon, this was of fibreglass construction throughout. The 15-38 was easily distinguished from its predecessor by a more streamlined nose and a T-tail. (en)
aspect ratio	20.600000 (xsd:double)
empty weight kg	230 (xsd:integer)
empty weight lb	507 (xsd:integer)
glide ratio	38 (xsd:integer)
gross weight kg	440 (xsd:integer)
gross weight lb	970 (xsd:integer)
height m	1.450000 (xsd:double)
length in	0 (xsd:integer)
length m	6.700000 (xsd:double)
max speed kmh	219 (xsd:integer)
max speed mph	136 (xsd:integer)
gold:hypernym	Sailplane
prov:wasDerivedFrom	wikipedia-en:CARMAM_15-38?oldid=1123003157&ns=0
page length (characters) of wiki page	2398 (xsd:nonNegativeInteger)
manufacturer	CARMAM
foaf:isPrimaryTopicOf	wikipedia-en:CARMAM_15-38
is Link from a Wikipage to another Wikipage of	CARMAM JP 15-38 CARMAM
is Wikipage redirect of	CARMAM JP 15-38
is foaf:primaryTopic of	wikipedia-en:CARMAM_15-38

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