About: Samolot Sp.I

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An Entity of Type : dbo:Aircraft, 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%2FSamolot_Sp.I&invfp=IFP_OFF&sas=SAME_AS_OFF

The low-powered Samolot Sp.I, designed in Poland in the mid-1920s, was intended to explore the characteristics of a proposed single seat fighter. The project did not receive government support and only one Sp.1 was built.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft aircraft
rdfs:label	Samolot Sp.I (en)
rdfs:comment	The low-powered Samolot Sp.I, designed in Poland in the mid-1920s, was intended to explore the characteristics of a proposed single seat fighter. The project did not receive government support and only one Sp.1 was built. (en)
foaf:depiction
dcterms:subject	1920s Polish experimental aircraft Samolot aircraft Single-engined tractor aircraft Parasol-wing aircraft
Wikipage page ID	55887204 (xsd:integer)
Wikipage revision ID	1075824383 (xsd:integer)
Link from a Wikipage to another Wikipage	Samolot Elevator (aeronautics) Monoplane 1920s Polish experimental aircraft Radial engine Bracing (aeronautics) Samolot aircraft Plywood Spar (aeronautics) Single-engined tractor aircraft Aircraft fairing Fighter aircraft PWS-10 Parasol wing Trailing edge Parasol-wing aircraft Landing gear Cockpit Tailplane Poland Cabane strut Rudder Salmson 9AC Semi-monocoque Poznan Salmson 9Ac Anzani 6 Fin (aeronautics)
sameAs	Samolot Sp.I Samolot Sp.I
span m	8.920000 (xsd:double)
wing area sqm	15 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Reflist dbt:Aircraft_specs dbt:Infobox_Aircraft_Type
thumbnail	wiki-commons:Special:FilePath/Samolot_SP.I_Annuaire_de_L'Aéronautique_1931.jpg?width=300
dbp:primeUnits%3F_	met (en)
first flight	July 1926 (en)
national origin	Poland
crew	One (en)
designer	Piotr Tulacz (en)
manufacturer	Samolot
ref	Cynk (en)
type	Single seat research aircraft (en)
has abstract	The low-powered Samolot Sp.I, designed in Poland in the mid-1920s, was intended to explore the characteristics of a proposed single seat fighter. The project did not receive government support and only one Sp.1 was built. (en)
airfoil	Dewoitine 26A (en)
empty weight kg	530 (xsd:integer)
eng1 hp	120 (xsd:integer)
eng1 name	Salmson 9AC
eng1 number	1 (xsd:integer)
eng1 type	9 (xsd:integer)
gross weight kg	715 (xsd:integer)
height m	2.300000 (xsd:double)
length m	6.100000 (xsd:double)
max speed kmh	190 (xsd:integer)
more performance	*Landing speed: (en)
number built	1 (xsd:integer)
prop blade number	2 (xsd:integer)
prov:wasDerivedFrom	wikipedia-en:Samolot_Sp.I?oldid=1075824383&ns=0
page length (characters) of wiki page	6748 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)
manufacturer	Samolot
origin	Poland
foaf:isPrimaryTopicOf	wikipedia-en:Samolot_Sp.I
is Link from a Wikipage to another Wikipage of	Samolot
is foaf:primaryTopic of	wikipedia-en:Samolot_Sp.I

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