About: SIPA Antilope

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An Entity of Type : yago:Whole100003553, 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%2FSIPA_Antilope

The SIPA S.251 Antilope was a low-wing monoplane, seating four or five and powered by a single turboprop engine, developed in France in the early 1960s. It set a number of class records but was not put into production.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft yago:Aircraft102686568 yago:Artifact100021939 yago:Conveyance103100490 yago:Craft103125870 yago:Instrumentality103575240 yago:Object100002684 yago:PhysicalEntity100001930 aircraft yago:Vehicle104524313 yago:Whole100003553
rdfs:label	SIPA S.251 (de) SIPA Antilope (en)
rdfs:comment	Die SIPA S.251 Antilope war ein Reiseflugzeug des französischen Herstellers Société industrielle pour l’aéronautique und wurde in den frühen 1960er Jahren entwickelt. (de) The SIPA S.251 Antilope was a low-wing monoplane, seating four or five and powered by a single turboprop engine, developed in France in the early 1960s. It set a number of class records but was not put into production. (en)
foaf:depiction
dcterms:subject	SIPA aircraft Low-wing aircraft Single-engined turboprop aircraft Single-engined tractor aircraft Aircraft first flown in 1962 1960s French civil utility aircraft
Wikipage page ID	28140419 (xsd:integer)
Wikipage revision ID	1075854513 (xsd:integer)
Link from a Wikipage to another Wikipage	NACA airfoil Monoplane SIPA aircraft Trim tab Low-wing aircraft Single-engined turboprop aircraft Turbomeca Astazou Single-engined tractor aircraft France Paris Air Show Fowler flaps Aircraft first flown in 1962 1960s French civil utility aircraft Société Industrielle Pour l’Aéronautique Turbomeca Astazou X Turboprop engine dbr:Ratier-Figeac
Link from a Wikipage to an external page	https://archive.org/stream/Aviation_Week_1963-06-24%23page/n48/mode/1up
sameAs	SIPA Antilope SIPA Antilope SIPA Antilope SIPA Antilope SIPA Antilope
span m	11.110000 (xsd:double)
wing area sqm	16.210000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_journal dbt:Commons_category dbt:Cvt dbt:Infobox_aircraft_type dbt:Refbegin dbt:Refend dbt:Reflist dbt:Aircraft_specs dbt:SIPA_aircraft
thumbnail	wiki-commons:Special:FilePath/SIPA_Antilope_F-BJSS_LBG_19.06.65_edited-2.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	1962-11-07 (xsd:date)
national origin	France
capacity	4 (xsd:integer)
crew	1 (xsd:integer)
manufacturer	Société Industrielle Pour l’Aéronautique
ref	Jane's All the World's Aircraft 1966-67 . (en)
status	stored in a private museum (en)
type	4 (xsd:integer)
has abstract	Die SIPA S.251 Antilope war ein Reiseflugzeug des französischen Herstellers Société industrielle pour l’aéronautique und wurde in den frühen 1960er Jahren entwickelt. (de) The SIPA S.251 Antilope was a low-wing monoplane, seating four or five and powered by a single turboprop engine, developed in France in the early 1960s. It set a number of class records but was not put into production. (en)
airfoil	root: NACA 23015; tip: NACA 4411 (en)
ceiling m	1100 (xsd:integer)
climb rate ms	13.500000 (xsd:double)
climb rate note	at sea level (en)
cruise speed kmh	380 (xsd:integer)
cruise speed note	70 (xsd:integer)
empty weight kg	990 (xsd:integer)
eng1 name	Turbomeca Astazou X
eng1 number	1 (xsd:integer)
eng1 shp	665 (xsd:integer)
eng1 type	turboprop (en)
height m	2.600000 (xsd:double)
length m	9.015000 (xsd:double)
max speed kmh	450 (xsd:integer)
max speed note	at (en)
max takeoff weight kg	1900 (xsd:integer)
number built	1 (xsd:integer)
prop blade number	3 (xsd:integer)
prop dia m	1.920000 (xsd:double)
prop dia note	constant-speed propeller (en)
prop name	Ratier-Figeac FH 76 (en)
range km	2000 (xsd:integer)
range note	typical max (en)
gold:hypernym	Monoplane
prov:wasDerivedFrom	wikipedia-en:SIPA_Antilope?oldid=1075854513&ns=0
page length (characters) of wiki page	7557 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)

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