About: Yakovlev Yak-141

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About: Yakovlev Yak-141 Sponge Permalink

An Entity of Type : dbkwik:resource/AGhloO_nVTaFp7GvOmHv5Q==, within Data Space : 134.155.108.49:8890 associated with source dataset(s)

The Yakovlev Yak-141 (; NATO reporting name "Freestyle"), also known as the Yak-41, was a supersonic vertical takeoff/landing (VTOL) fighter aircraft designed by Yakovlev. It did not enter production.

Attributes	Values
rdf:type	Aircraft Type
rdfs:label	Yakovlev Yak-141
rdfs:comment	The Yakovlev Yak-141 (; NATO reporting name "Freestyle"), also known as the Yak-41, was a supersonic vertical takeoff/landing (VTOL) fighter aircraft designed by Yakovlev. It did not enter production. Development of the Yak-141 started in the year 1975, at this time it was called Yak-41. It was developed from the Yakovlev Yak-38. The first conventional flight took place on 9th March 1987 and the first hovering flight was made on 29th December 1989. The main role of the aircraft was to be air defense of the fleet. Its flight performance and avionic systems were known to be similar to those of the current fighters of this time. The afterburning, vectoring main engine of the Yak-141 was mounted on the rear part of the fuselage. In the year 1991 it was renamed to Yak-141.
sameAs	dbr:Yakovlev_Yak-141
dcterms:subject	Jet aircraft Russian Aircraft dbkwik:resource/jzdbnoF7gtt9JMuMxn65Cg== Fighters dbkwik:resource/MzMDPQPUMFxKjFJFx6LfsQ== dbkwik:resource/cWlE4zDh_2O5CNnbLlM_cg== dbkwik:resource/dE4SR41P3VcvZpsifT_bpQ== dbkwik:resource/TYysmSnxcwDuBaOqXGGSXA== dbkwik:resource/pJ4Bb9votdwC4h3IZV5IhA== dbkwik:resource/9rh1gF7JXSY5VfZAdOI4gA== dbkwik:resource/tNDrA85DvL_7GZoFXjpONA== dbkwik:resource/I8m8l8BXokzxXCfnv090wQ== dbkwik:resource/A9p1MJUCwPxlYPUKCRNfHQ==
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max takeoff weight alt	42989.0
hardpoint capacity	2600(xsd:integer)
Guns	1(xsd:integer)
climb rate main	15000(xsd:integer)
length alt	60(xsd:integer)
span main	10.105 m
Status	Cancelled in August 1991
thrust alt	24300(xsd:integer)
height alt	500.38
primary user	Soviet Navy
Type	VTOL fighter
range alt	1305.0
length main	18.36 m
area main	31.7
ferry range main	3000.0
hardpoints	4(xsd:integer)
height main	5.00 m
hardpoint missiles	R-73 Archer, R-77 Adder or R-27 Alamo air-to-air missiles
span alt	33(xsd:integer)
range main	2100.0
Manufacturer	Yakovlev
max speed main	1800.0
climb rate alt	49213.0
ceiling main	15,500 m
afterburning thrust main	152 kN
empty weight main	11650.0
afterburning thrust alt	34170(xsd:integer)
type of jet	lift/cruise turbofan
area alt	341.0
First Flight	1987-03-09(xsd:date)
engine (jet)	MNPK Soyuz R-79V-300
max speed alt	1118(xsd:integer)
jet or prop?	jet
ferry range alt	1865.0
empty weight alt	25683.0
thrust main	108 kN
number of jets	1(xsd:integer)
plane or copter?	plane
ceiling alt	50853.0
max takeoff weight main	19500.0
Crew	1(xsd:integer)
Number Built	2(xsd:integer)
ref	Yakovlev data, Gunston, Winchester, Wilson
abstract	The Yakovlev Yak-141 (; NATO reporting name "Freestyle"), also known as the Yak-41, was a supersonic vertical takeoff/landing (VTOL) fighter aircraft designed by Yakovlev. It did not enter production. Development of the Yak-141 started in the year 1975, at this time it was called Yak-41. It was developed from the Yakovlev Yak-38. The first conventional flight took place on 9th March 1987 and the first hovering flight was made on 29th December 1989. The main role of the aircraft was to be air defense of the fleet. Its flight performance and avionic systems were known to be similar to those of the current fighters of this time. The afterburning, vectoring main engine of the Yak-141 was mounted on the rear part of the fuselage. In the year 1991 it was renamed to Yak-141. The Yak-141 can reach speeds of about Mach 1.7 and was to be as agile as the Mikoyan MiG-29. The program was cancelled in August 1991. The technologies developed for the fully traversable engine were used in the United States for development of the F135 engine (engine of the F-35) by Pratt & Whitney.

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