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The Mitsubishi AAM-5 (Type 04 air-to-air missile, 04式空対空誘導弾) is a short-range air-to-air missile developed and produced by Mitsubishi Heavy Industries for the Japan Air Self-Defense Force. Development of the missile as a replacement for the AAM-3 (Type 90) missile commenced in 1991 and it has been operational since 2004.
 | This article does not cite any sources. (March 2007) |
| AAM-5 | |
|---|---|
 AAM-5 and AAM-5B | |
| Type | air-to-air |
| Place of origin | Japan |
| Service history | |
| In service | 2004 - present |
| Used by | Japan Air Self-Defense Force |
| Production history | |
| Manufacturer | Mitsubishi Heavy Industries |
| Unit cost | 55-60 million yen |
| Specifications | |
| Mass | 95 kg (209 lb) |
| Length | 3.105 m (10.19 ft) |
| Diameter | 130 mm (5.1 in) |
| Warhead | blast-frag |
Detonation mechanism | laser proximity fuze and impact |
| Wingspan | 440 mm (17 in) |
| Propellant | solid fuel rocket |
Operational range | 35 km (22 mi) |
| Maximum speed | Mach 3 |
Guidance system | (Infrared homing (IIR) INS+COLOS) (B version (IRCCM) INS+COLOS) |
Characteristics
Unlike the Type 90 guided missile, the AAM-5 does not have canard control surfaces, using thrust vectoring for high agility. The missile body has narrow strakes extending over most of its length.
The NEC manufactured seeker has also been improved. Addition of a triaxial gimbal to the infrared seeker has increased the field of view and an infrared focal plane array multi-element seeker allows infrared imaging. In particular, the addition of an INS means mid-course updates and LOAL (Lock-on after launch) is possible. Terminal homing is via infrared imaging (IIR). In terms of generation, it is placed in the same generation as missiles such as the AIM-9X and IRIS-T.
Variants
- AAM-5
- Standard.
- AAM-5B
- Enhanced background discrimination capability and IRCCM. Seeker cooling time is extended by the adoption of a Stirling engine.
Operators
Japan
- Japan Air Self-Defense Force
Gallery
Dummy
Seeker
Thrust vectoring Nozzle
Specifications
- Length: 3,105 mm
- Diameter: 130 mm
- Wing span: 440 mm
- Weight: 95 kg
- Guidance: AAM-5A: Terminal Infrared homing (IIR), INS+COLOS
- Guidance: AAM-5B: Terminal IIR with IRCCM, INS+COLOS)
- Warhead: blast fragmentation warhead
- Detonation Mechanism: laser proximity fuze and impact
- Range: 35 km
- Speed: Mach 3+
See also
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На других языках
[de] Mitsubishi AAM-5
Die von Mitsubishi Heavy Industries entwickelte AAM-5 ist eine Kurzstrecken-Luft-Luft-Rakete, die sich zurzeit in der Erprobungsphase (XAAM-5) befindet. Es war geplant, dass die AAM-5 im Jahr 2008 in Dienst gestellt wird und dann schrittweise die AAM-3 ersetzt. Die Waffe ist der IRIS-T sehr ähnlich.- [en] AAM-5 (Japanese missile)
[it] Mitsubishi AAM-5
Il Mitsubishi AAM-5 (Type 04, Maruyon Shiki Kūtaikū Yūdōdan, 04式空対空誘導弾) è un missile aria-aria a guida infrarossa, prodotto dalla Mitsubishi Heavy Industries ed entrato in servizio nel 1991 nella Kōkū Jieitai, dove fu installato sui caccia McDonnell Douglas F-15J Eagle, e sul cacciabombardiere Mitsubishi F-2.[ru] Mitsubishi AAM-5
Тип 04 (яп. 04式空対空誘導弾 04 сики ку:таику: ю:до:дан, «управляемая ракета воздух-воздух типа 04», также Мицубиси AAM-5 (англ. Mitsubishi Air-to-Air Missile 5)) — японская управляемая ракета класса «воздух—воздух» малой дальности, оснащённая тепловой головкой самонаведения. Разработка корпорации Mitsubishi Heavy Industries, на 2007 год находилась в финальной стадии испытаний (прототип XAAM-5) и принятия на вооружение. По характеристикам близка к европейской IRIS-T. В Воздушных силах самообороны Японии должна постепенно заменить ракеты AAM-3 предыдущего поколения.Другой контент может иметь иную лицензию. Перед использованием материалов сайта WikiSort.org внимательно изучите правила лицензирования конкретных элементов наполнения сайта.
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