About: Kuznetsov NK-22

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The Kuznetsov NK-22 is an afterburning turbofan engine, designed by the Kuznetsov Design Bureau.

Attributes	Values
rdfs:label	Kuznetsov NK-22 (en) НК-22 (ru)
rdfs:comment	The Kuznetsov NK-22 is an afterburning turbofan engine, designed by the Kuznetsov Design Bureau. (en) НК-144-22 (изделие «ФМ») — двухконтурный, двухкаскадный турбореактивный двигатель с форсажной камерой (ТРДДФ), разработанный на Куйбышевском моторном заводе под руководством Н. Д. Кузнецова. Испытания начались в 1968 году. Серийно производился с 1969 по 1984 годы. (ru)
dcterms:subject	Kuznetsov aircraft engines 1960s turbofan engines Low-bypass turbofan engines
Wikipage page ID	68889598 (xsd:integer)
Wikipage revision ID	1110472347 (xsd:integer)
Link from a Wikipage to another Wikipage	Kuznetsov aircraft engines List of aircraft engines 1960s turbofan engines Low-bypass turbofan engines Kuznetsov Design Bureau Kuznetsov NK-144 Tupolev Tu-144 Tupolev Tu-22M Turbofan Afterburner Aviation fuel Soviet Union Kuznetsov NK-25 Supersonic transport Tupolev Tu-22M2 Tu-22M
sameAs	Kuznetsov NK-22 Kuznetsov NK-22 Kuznetsov NK-22
similar engines	*Kuznetsov NK-25 (en)
specfuelcon	1.950000 (xsd:double)
thrust	with full afterburner in cruise (en)
turbine	3 (xsd:integer)
dbp:wikiPageUsesTemplate	dbt:Kuznetsov_aeroengines dbt:Cvt dbt:Reflist dbt:Short_description dbt:Jetspecs dbt:Aircontent dbt:Infobox_Aircraft_Engine dbt:Aeroengine-specs
national origin	Soviet Union
manufacturer	Kuznetsov Design Bureau
ref	airwar.ru and leteckemotory.cz (en)
type	Turbofan Two-spool low-bypass afterburning turbofan (en)
has abstract	The Kuznetsov NK-22 is an afterburning turbofan engine, designed by the Kuznetsov Design Bureau. (en) НК-144-22 (изделие «ФМ») — двухконтурный, двухкаскадный турбореактивный двигатель с форсажной камерой (ТРДДФ), разработанный на Куйбышевском моторном заводе под руководством Н. Д. Кузнецова. Испытания начались в 1968 году. Серийно производился с 1969 по 1984 годы. (ru)
bypass	0.600000 (xsd:double)
combustion	Annular multi-nozzle combustion chamber (en)
compression	14.750000 (xsd:double)
compressor	12 (xsd:integer)
developed from	Kuznetsov NK-144
developed into	NK-23 (en)
first run	April 1968 (en)
fueltype	T-7 or RT kerosene type fuel (en)
lists	*List of aircraft engines (en)
major applications	Tupolev Tu-22M
prov:wasDerivedFrom	wikipedia-en:Kuznetsov_NK-22?oldid=1110472347&ns=0
page length (characters) of wiki page	5097 (xsd:nonNegativeInteger)
foaf:isPrimaryTopicOf	wikipedia-en:Kuznetsov_NK-22
is Link from a Wikipage to another Wikipage of	List of aircraft engines Kuznetsov Design Bureau Kuznetsov NK-144 JSC Kuznetsov Kuznetsov NK-25 Kuznetsov NK-6
is developed into of	Kuznetsov NK-144
is foaf:primaryTopic of	wikipedia-en:Kuznetsov_NK-22

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