2017년 1월 26일 목요일

Yak-130 (plane)

Yak-130 (plane)

Yak-130

Yak-130 in MAKS of 2009

Yak-130 in MAKS of 2009

Yak-130 (Russianк-130) is Russian double seats high jet training plane / light air raider that made the first flight on April 26, 1996. The NATO code name "ミットン" (Mitten).

Table of contents

Summary

Development

 
Mock-up of the body pit exhibited in MAKS of 2013

In Yak-130, アエロ L-29 and L-39 which got a duty in Soviet Union Air Force and Soviet Union Navy flying corps planned in the 1980s were designed depending on demand specifications (as for the navy flying corps use from a carrier conditioning of the use) of 200 new high grade training plane to substitute. In consideration of lack of funds and overseas export, the tie-up of the overseas maker is explored from the beginning of plan and succeeds in the agreement conclusion with the Italian Aer Macchi (existing array near Aer Macchi) company which demanded a new trainer in the same way in 1987.

Five designs station (OKB) designed it depending on this demand specifications, and at first S-54 plan of the Sukhoi design station and a plan of another design station fell off it, and subsequently the M-200 plan of the ミャスィーシチェフ design station was taken off, and it was competition trial manufacture of Yak-UTK plan (with Yak-UTS) and the MiG-AT plan of the Mikoyan グレヴィッチ design station (with thing, MiG-UTS which I canceled an unpopular initial plan and suggested again) of the Aleksander Yakovlev design station.

It was subsonic speed, but Yak-UTK which was the design that was more advanced than MiG-AT of the straight line wing was adopted and was finally named Yak-130. The Aer Macchi company version was referred to AEM-130 at first, but I was changed to M-346 later and came to be performed from a design to sale hardly separately (later description).

With joint development with Aer Macchi company, the Aleksander Yakovlev performed a common enterprise by the development of the Yak-141 VTOL fighter with Lockheed Martin Corporation and decided it in the Aleksander Yakovlev developing the high subsonic speed training plane that could program longitudinal stability from plus to some minus number.

According to the early plan, this machine was a body similar to ダッソーラファール where the air inlet of the engine lengthened to the lower area of the cockpit. This design was changed for from 1993 to 1994, and the air inlet was moved on the body side, and a supporting inlet port was added to the upper part of the inlet port of right and left like a MiG-29. An engine vent is wrapped in afterbody squeezed keenly at the rear.

I keep an opening and shutting-type cover in the air inlet to prevent the alien substance inhalation to an engine running on above the ground and use it in combination with an assistance inlet port of the body back.

Two engines are equipped with under the root of the main wing lengthened to a canopy for a long time forward. Originally イーウチェンコ AI-25 engine was chosen, but I was changed to クリーモフ RD-35M (DV-2S) which produced a thrust of 2,200 kg (4,850lbs) later, and it was equipped by a demonstrator machine. It finally became the AI-2222-25 engine which produced a thrust of 2,520 kgf (5,552lbf) with the mass production type. Engine control is FADEC, and AI-222 is available for the careful adjustment of the thrust and contributes to mobility. The plane member is made of metal, but a composite is used widely to be able to tolerate the use of 25,000 hours from 15,000.

A wingtip has a tall wing let on the main wing of the delta wing of the sweepback of 31 degrees in a leading edge, and all buckets are power operation types. The internal fuel burden can attach a body coherence type belly tank of 700L in capacity (154 gal) to the body undersurface at 2,060L (454 gal).

The undercarriage uses low-pressure Thai a peculiar to Aleksander Yakovlev in consideration of the use from the unpaved runway, and, as for the front wheel which can steer a ship, the main wheel is drawn into the cover part of the duct for the engine inlet port to the rear.

The big canopy is a wide difference type, and the big front part shelter belt is slanted forward. I keep the multifunctional display of 3 screens in the backseat in front of the supercharge-type cockpit with navigation and the head up display (HUD) for the weapon aim and equip both seats with K-36 ejector seat made in ズヴェズダ of zero / zero method.

I comprise the thing which automated on board diagnosis / control system and simplify use and maintenance.

I can put a guided missile and a variety of weapons including the cancer pod on seven places of outside hard points.

Test

 
Yak-130 in MAKS of 1997

The trial manufacture first issue machine which could not fly was released on November 30, 1994, and it was announced that they were made of Aleksander Yakovlev, but all development programs were common enterprises with Italian Aer Macchi company. This body was displayed by Paris airshow again in June, 1995. This plane finally made the first flight in ジュコーフスキー) on April 15, 1996.

Aer Macchi company and the Aleksander Yakovlev did not reach the agreement with the last design specifications after maiden flight soon, and the common enterprise of both was finished. All Aer Macchi company developed M-346 which they improved to be able to start high speed at the expense of a flying range to some extent using the parts of the Western countries while Aleksander Yakovlev pushed forward development of Yak-130 of the original design.

Yak-130 stood out in the Kremlin for vying in 1998 and announced that I placed an order for 200 planes. Because a development period was prolonged by lack of funds, the first mass production specifications airplane made the first flight on April 30, 2004.

Characteristic

I can let you learn the fourth, fourth .5, the flying method of the fifth generation fighter for a flight trainee in time having a short it because Yak-130 can reproduce the flight characteristic of the fourth .5 generations machine by mechanism represented by the fried food by wire which kept four folds of long-windedness to raise flight safety and superiority of the ability for battle.

The sky vs. sky and an air-to-ground missile, bomb throwing down, a cannon and the simulation of the air self-defense system and practical discharge are included in weapon training in Yak-130. The instructor can perform setting and the control of "the target action" while being on board.

Derivation type

Yak/AEM-130D
A demonstrator by the Aleksander Yakovlev & Italy Aer Macchi cooperation development. It is the model machine that flight off with MiG-AT became the biggest purpose. Italy company leaves development only in this.
Yak-130
Double seats high training plane type
Yak-131
Light fighter type
Yak-133
The pattern of the development type. It is suggested by a name of Yak-133 in succeeding plane of Su-25 plan (LUS).
Yak-133IB
Battle bombing model
Yak-133PP
Electronic interference type
Yak-133R
Reconnaissance type
Yak-135
4 seat VIP carrier [1] models

Operational

  Russia
Russian air force
I made 55 contracts in December, 2011 [2] and contracted 22 planes more in December, 2013 [3]. I made 30 contracts newly in April, 2016 [4]. I finally expect 200 deployment [5].
The Russian navy
I make a contract to introduce first five planes in December, 2013 and am going to finally deploy ten planes [6].
  Algeria
Various notation such as caution data or the cockpit of the body becomes English in 16 ordering, Yak-130 of Algerian specifications [7].
  Bangladesh
I place an order for 24 planes [8].
  Syria
I place an order for 36 planes [9]

Essential points (Yak-130)

The source: www.yak.ru[10]

Specifications

  • A crew: Two people
  • Full length: 11.49m (37 ft 8 in)
  • Overall height: 4.76m (15 ft 7 in)
  • Wingspread: 9.72m (31 ft 10 in)
  • A wing area: 63.5m2 (683.5 ft2)
  • Wing type: 63.5m2 (683.5 ft2)
  • Emptiness weight: 4,600 kg (10,141 lb)
  • Operational time weight: 6,350 kg (14,000 lb)
  • Maximum takeoff weight: 10,290 kg (22,685 lb)
  • Power: イーウチェンコ AI-222-25 turbofan, 21.58 kN (4,852 lbf) *2

Performance

  • Maximum velocity: 1,037km/h (644mph)
  • Cruising speed: 887km/h (551mph)
  • Stalling speed: 165km/h (103mph)
  • A flying range: 2,546km (1,582 miles)
  • The rate of climb: 50m/s (10,000 ft/min)
  • Loading: 276.4 kg/m2 (56.60 lb/sq ft)
  • The thrust weight ratio: 0.78

Armament

  • I divide it into nine hard points and can be equipped with a weapon made in Russia of 3,000 kg in total.
  As for the commentary of the used unit, please see Wiki project aviation / physics unit.

Allied item

Source

Outside link


This article is taken from the Japanese Wikipedia Yak-130 (plane)

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