About: Yakovlev Ya-21

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http://dbpedia.org/describe/?url=http%3A%2F%2Fdbpedia.org%2Fresource%2FYakovlev_Ya-21

The Yakovlev Ya-21, (aka UT-21, No.21 or No.25), was a single-seat high-speed sport aircraft / fighter-trainer designed and built in the Soviet Union in the late 1930s.

Attributes	Values
rdf:type	Thing schema:Product mean of transportation Aircraft aircraft
rdfs:label	Yakovlev Ya-21 (en)
rdfs:comment	The Yakovlev Ya-21, (aka UT-21, No.21 or No.25), was a single-seat high-speed sport aircraft / fighter-trainer designed and built in the Soviet Union in the late 1930s. (en)
dcterms:subject	Low-wing aircraft Single-engined tractor aircraft 1930s Soviet sport aircraft Aircraft first flown in 1937 Yakovlev aircraft
Wikipage page ID	54637786 (xsd:integer)
Wikipage revision ID	1029827629 (xsd:integer)
Link from a Wikipage to another Wikipage	Renault 4P Machine gun Low-wing aircraft USSR Single-engined tractor aircraft 1930s Soviet sport aircraft Aircraft first flown in 1937 Yakovlev UT-1 Soviet Union Yakovlev aircraft Shvetsov M-11 Yakovlev AIR-18 Yakovlev BB-22 Yakovlev I-26 ShKAS Renault 6Q-01 OKB Yakovlev Voronezh MV-6 dbr:Kossov_MG-31F
sameAs	Yakovlev Ya-21 Yakovlev Ya-21
span m	7.800000 (xsd:double)
time to altitude	450.0 (second)
wing area sqm	9.580000 (xsd:double)
dbp:wikiPageUsesTemplate	dbt:Convert dbt:Infobox_aircraft_type dbt:Reflist dbt:Aircraft_specs dbt:Yakovlev_aircraft
dbp:primeUnits%3F_	met (en)
first flight	September 1937 (en)
national origin	USSR
crew	1 (xsd:integer)
fuel capacity	/ fuel; oil (en)
manufacturer	OKB Yakovlev
ref	OKB Yakovlev, Yakovlev aircraft since 1924 (en)
type	single-seat fighter-trainer / high-speed sport aircraft (en)
has abstract	The Yakovlev Ya-21, (aka UT-21, No.21 or No.25), was a single-seat high-speed sport aircraft / fighter-trainer designed and built in the Soviet Union in the late 1930s. (en)
airfoil	Göttingen 387 (en)
armament	* 1x fixed forward firing synchronised 7.62mm ShKAS machine gun (en)
ceiling m	7000 (xsd:integer)
cruise speed kmh	290 (xsd:integer)
developed from	Yakovlev UT-1
empty weight kg	611 (xsd:integer)
eng1 hp	220 (xsd:integer)
eng1 name	Renault 6Q-01
eng1 number	1 (xsd:integer)
eng1 type	6 (xsd:integer)
height m	2.050000 (xsd:double)
length m	6.400000 (xsd:double)
max speed kmh	290 (xsd:integer)
max speed note	at sea level at *Landing speed: with flaps, no flaps (en)
max takeoff weight kg	831 (xsd:integer)
more performance	Take-off run: Landing run: (en)
number built	1 (xsd:integer)
prop blade number	2 (xsd:integer)
prop dia m	2.100000 (xsd:double)
prop name	fixed pitch wooden propeller (en)
range km	715 (xsd:integer)
prov:wasDerivedFrom	wikipedia-en:Yakovlev_Ya-21?oldid=1029827629&ns=0
page length (characters) of wiki page	5741 (xsd:nonNegativeInteger)
number built	1 (xsd:nonNegativeInteger)
manufacturer	OKB Yakovlev
origin	USSR
predecessor	Yakovlev UT-1
foaf:isPrimaryTopicOf	wikipedia-en:Yakovlev_Ya-21
is Link from a Wikipage to another Wikipage of	List of aircraft (Y) Yakovlev UT-21
is Wikipage redirect of	Yakovlev UT-21
is foaf:primaryTopic of	wikipedia-en:Yakovlev_Ya-21

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