About: SIPA S.300

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An Entity of Type : yago:Whole100003553, 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%2FSIPA_S.300&invfp=IFP_OFF&sas=SAME_AS_OFF

The SIPA S.300 was a French turbojet powered basic trainer, claimed to be the first of its kind anywhere. Only one was built, the prototype crashing after a year's development.

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.300 (de) SIPA S.300 (en)
rdfs:comment	Die SIPA S.300 war ein leichtes strahlgetriebenes Schulflugzeug des französischen Herstellers Société industrielle pour l’aéronautique. (de) The SIPA S.300 was a French turbojet powered basic trainer, claimed to be the first of its kind anywhere. Only one was built, the prototype crashing after a year's development. (en)
dcterms:subject	SIPA aircraft Low-wing aircraft Single-engined jet aircraft Aircraft first flown in 1954 1950s French aircraft
Wikipage page ID	31640694 (xsd:integer)
Wikipage revision ID	1107909720 (xsd:integer)
Link from a Wikipage to another Wikipage	Monoplane SIPA aircraft Elevator (aircraft) Liaison aircraft Low-wing aircraft Trainer (aircraft) Turbomeca Aspin Turbomeca Marboré Turbomeca Palas Fin France Dorsal (anatomy) Single-engined jet aircraft Aircraft first flown in 1954 Suresnes 1950s French aircraft Wing configuration Société Industrielle Pour l’Aéronautique Fillet (mechanics) Air brake (aircraft) Canopy (aircraft) Hydraulic Rudder Turbojet SIPA S.200 Minijet Ventral Balanced dbr:Turbomeca_Super_Palas
Link from a Wikipage to an external page	http://www.aviafrance.com/s-i-p-a-s-300r-aviation-france-1163.htm%7Ctitle=SIPA
sameAs	SIPA S.300 SIPA S.300 SIPA S.300 SIPA S.300 SIPA S.300
span m	8.020000 (xsd:double)
wing area note	gross (en)
wing area sqm	9.800000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Cite_journal dbt:Cite_web dbt:Commons_category dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircontent dbt:Aircraft_specs dbt:SIPA_aircraft
dbp:primeUnits%3F_	met (en)
first flight	1954-10-04 (xsd:date)
national origin	France
capacity	2 (xsd:integer)
designer	Yves Gardan (en)
fuel capacity	210 (xsd:integer)
group	Notes (en)
manufacturer	Suresnes Société Industrielle Pour l’Aéronautique
ref	Jane's All the World's Aircraft 1956/7 (en)
type	Jet primary trainer and liaison aircraft (en)
has abstract	Die SIPA S.300 war ein leichtes strahlgetriebenes Schulflugzeug des französischen Herstellers Société industrielle pour l’aéronautique. (de) The SIPA S.300 was a French turbojet powered basic trainer, claimed to be the first of its kind anywhere. Only one was built, the prototype crashing after a year's development. (en)
ceiling m	5050 (xsd:integer)
climb rate ms	4.500000 (xsd:double)
cruise speed kmh	312 (xsd:integer)
empty weight kg	583 (xsd:integer)
eng1 kn	1.570000 (xsd:double)
eng1 name	Turbomeca Palas
eng1 number	1 (xsd:integer)
eng1 type	centrifugal turbojet (en)
gross weight kg	920 (xsd:integer)
height m	2.570000 (xsd:double)
length m	6.710000 (xsd:double)
max speed kmh	360 (xsd:integer)
number built	1 (xsd:integer)
range km	450 (xsd:integer)
gold:hypernym	Turbojet
prov:wasDerivedFrom	wikipedia-en:SIPA_S.300?oldid=1107909720&ns=0
page length (characters) of wiki page	9464 (xsd:nonNegativeInteger)

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