2016년 9월 7일 수요일

Kh-25 (missile)

Kh-25 (missile)

Kh-25ML/MLT/MR
(NATO identification name: AS-10 Karen)
Kh-25MP (AS-12 Kegler)

Kh-25ML.jpg
Kh-25ML
Kind Tactics air-to-ground missile
Anti-radar missile (Kh-25MP)
Original development country Flag of the Soviet Union The Soviet Union
The operational history
Deployment period As of 1975 -
Deployment Russian flag Russia
History of development
Development period From 1971 to 1975
Manufacturer Zvezda-Strela
Specifications
Weight Kh-25ML: 299 kg (659 lb)[1]
Kh-25MP: 315 kg (694 lb)[2]
Full length Kh-25ML: 370.5cm (12 ft 2 in)[1]
Kh-25MP 1VP: 425.5cm (167.5 in)[2]
Kh-25MP 2VP: 435.5cm (171.5 in)[2]

Diameter 27.5 cm (10.8 in)[1]

Warhead High explosive, shell form
Quantity of bursting charge Kh-25MP: 86 kg (190 lb)[2]

Wingspread 75.5 cm (29.7 in)[1]
Instruction method It is laser, passive radar, TV, IR, satnav, Acty braider by a derivation model
Discharge
Platform
A MiG-21, it is Su-17/20/22,[3] Su-24,[3] Su-25,[3] Su-27[3] MiG-23/27,[3] MiG-29 [3] [3]
Kh-25MP: MiG-23/27,[4] Su-17/22,[4] Su-24,[4] Su-25[4]

The second generation tactics air-to-ground missile of the Soviet Union (Russia) where Kh-25 (Х-25, NATO code name AS-10 Karen) was developed from the end of 1960s through the 1970s. I seem to be an improved version of Kh-23/66Grom (NATO code name AS-7 Kerry) and resemble closely very much. I comprise modular-type guidance controls, and, as for the range, 10km is [1]. The derivation model of anti-radar missile specifications (Kh-25MP) is known as AS-12 Kegler in NATO, and, as for the range, up to 40km is [2]. Kh-25 designed by Zvezda-Strela is a model derived from Kh-23 (AS-7 Kerry) of laser guidance specifications. The Kh-38 series of the succeeding model inherits it, but Kh-25 is used widely now, too.

Table of contents

Development

Beam riding instruction-type Kh-66 that the air-to-air missile that use was started in 1968 was developed for the cause was air-to-surface missile for the first tactics plane for the Soviet Union [5]. However, it was necessary for the plane to make nose dive at the time of discharge, and use was accompanied with difficulty. Kh-23 which was an electric wave command guidance-type derivation model was examined for the first time in 1968, but I had a problem to guidance controls and needed five years by an operational start [6]. Therefore the work of the derivation model of the cicada active laser seeker was started in 1971 and became Kh-25 [5]. This was known as Kh-23L at first in the Western countries [7]. An examination was started on November 24, 1974, and a mass production contained Kh-25 from 1975 [5]. The work of the derivation model of anti-radar missile specifications from [5]Kh-66 using the passive seeker and SUR-73 automatic pilot was started in 1972 [4].

Kh-31 of the long range vs. the radar missile was done from the same plan, too [5]. I put the examination of Kh-27 on MiG-27 and was made a start [5] on August 8, 1975, but the operational start was September 2, 1980 [5]. The NATO identification name was AS-12 Kegler and rearranged Kh-28 (AS-9 Kyle) [4].

I started work to integrate Kh-23M, Kh-25 and Kh-27 with a single modular system that "Victor Bugaiskii" which was a chief engineer of the design station reduced an expense in 1973 and increased flexibility of the tactics [5]. This work was completed at the end of 1978 [5], and, as a result, Kh-25MP (anti-radar), Kh-25ML (laser guidance) and the Kh-25MR (electric wave instruction) series were possible. NATO appointed these sequentially now as AS-12 and AS-10 though I could easily change a seeker head.

Design

Kh-25 resembles a latter term model of Kh-23 closely in a canard and a wing of the cruciate very much.

A homing head is it in 1VP and 2VP2 kind, and Kh-25MP vs. the radar missile receives different frequency [2].

Operational results

Archetypal Kh-25 was put on MiG-23, MiG-27, Su-17M in Soviet Union Air Force for from 1973 to 1975, and use was started [3].

Thereafter it is confirmed to be used in MiG-21, MiG-29, Su-17/20/22 series, Su-24, Su-25, Su-27 [3]. A helicopter such as Ka-50 is equipped even with equally.

I can put Kh-25MP on MiG-23/27, Su-17/22, Su-24, Su-25 [4].

Data

  • Full length: 3.83m (MR), 4.255m (ML)
  • A diameter: 27.5cm
  • Wingspread: 82cm
  • A warhead: 140 kg of HE (MR), 89.6 kg of HE (ML)
  • An instruction method: Radio order (MR), cicada active laser (ML)
  • A range: 10km (MR), 20km (ML)
  • A design: The Zvezda design station
  • A main deployment machine: MiG-27Su-17Su-20Su-22Su-24Su-25

Version

NATO appoints all Kh-25 series except the anti-radar use as AS-10 Karen. "M" is abbreviation of the "Modulnaya" - module (seeker).

Kh-25 (Izdeliye 71, Kh-23L)
A laser guidance type to become the model.
Kh-25ML
A cicada active laser guidance type. I penetrate the concrete wall of 1 meter (39 in) of thickness in the thing with the double warhead [8].
Kh-25MA
An Acty braider instruction type. I was exported for the first time in 1999 [3].
Kh-25MAE
It was for update of Kh-25MA, and the export of specifications equipped with the seeker of the Ka- band in August, 2005 was announced. PSM of Phazotron company has the ability that the tank of the 4,000m (4,370 yd) distance is caught, and it is estimated that I am used for Kh-25MA [8].
Kh-25MS
It carries GPS or GLONASS satellite guidance controls [3].
Kh-25MSE
With an export of Kh-25MS type, I was announced in August, 2005 [8].
Kh-25MT
A TV instruction type [3].
Kh-25MTP
An imaging IR instruction type [3].
Kh-25R/Kh-25MR
An electric wave command guidance type [3].
Kh-27 (Kh-27/M, AS-12 Kegler)
The model model of the anti-radar missile.
Kh-25MP (AS-12 Kegler)
The module type vs. the radar missile [4].
Kh-25MPU (AS-12 Kegler)
Improved Kh-25MP[4].

As for the training bullet, "U" is appointed. There are the following models in Kh-25ML

Kh-25MUL
Kh-25ML[1] for the fight war training.
Kh-25ML-UD
A missile [1] for the function training.
Kh-25ML-UR
A missile [1] for the partial training.

Similar missile

Footnote

  1. ^ a b c d e f g h i j "Kh-25ML". Tactical Missiles Corporation (2004). 2010 reading....
  2. ^ a b c d e f g h "Kh-25MP". Tactical Missiles Corporation (2004). 2010 reading....
  3. ^ a b c d e f g h i j k l It is read m n "Kh-25" (AS-10 'Karen') on Jane's Air-Launched Weapons, (2008-08-01), http://www.janes.com/extracts/extract/jalw/jalw2917.html February 7, 2009.  [Broken link]
  4. It is read ^ a b c d e f g h i "Kh-25MP, Kh-25MPU" (AS-12 'Kegler') on Jane's Air-Launched Weapons, (2008-08-01), http://www.janes.com/articles/Janes-Air-Launched-Weapons/Kh-25MP-Kh-25MPU-AS-12-Kegler-Russian-Federation.html February 7, 2009. 
  5. ^ a b c d e f g h i (Word 97 DOC) History of JSC Tactical Missile Corporation, pp. 4–6, http://eng.ktrv.ru/docs/history_eng.doc February 26, 2009 reading. 
  6. ^ Friedman, Norman (1997), The Naval Institute Guide to World Naval Weapons Systems, Naval Institute Press, p. 235, ISBN 9781557502681, http://books.google.com/?id=l-DzknmTgDUC&pg=PA235&lpg=PA235 2010 reading....

This article is taken from the Japanese Wikipedia Kh-25 (missile)

This article is distributed by cc-by-sa or GFDL license in accordance with the provisions of Wikipedia.

Wikipedia and Tranpedia does not guarantee the accuracy of this document. See our disclaimer for more information.

In addition, Tranpedia is simply not responsible for any show is only by translating the writings of foreign licenses that are compatible with CC-BY-SA license information.

0 개의 댓글:

댓글 쓰기