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http://en.wikipedia.org/wiki/Aung_Zeya_class_frigate
General characteristics
Type: Frigate
Displacement: 4,053 tonnes (full), 3,600 tonnes (standard)
Length: 134 m (440 ft)
Beam: 16 m (52 ft)
Propulsion: CODAD, 4 x SEMT Pielstick 16 PA6 STC diesels, 5700 kW (7600+ hp @ 1084 rpm) each
Speed: 30 kn estimated
Range: 3,800 miles estimated
Sensors and
processing systems: Type 382 Radar ("Sea Eagle S/C") 3D air/surface search radar
Type 344 (Mineral-ME Band Stand) OTH target acquisition and SSM fire control radar
4 x Type 345 (MR-90 Front Dome) SAM fire control radars
MR-36A surface search radar, I-band
Type 347G 76 mm gun fire control radar
2 x Racal RM-1290 navigation radars, I-band
MGK-335 medium frequency active/passive sonar system
ZKJ-4B/6 (developed from Thomson-CSF TAVITAC) combat data system
HN-900 Data link (Chinese equivalent of Link 11A/B, to be upgraded)
SNTI-240 SATCOM
Electronic warfare
and decoys: Type 922-1 radar warning receiver
HZ-100 ECM & ELINT system
Armament: 1 x HQ-16 32-cell VLS SAM launcher
8 x HN-2 land attack cruise missiles [1]
2 x 4 C-803 anti-ship / land attack cruise missiles
1 x 76 mm dual purpose gun
2 x Type 730 7-barrel 30 mm CIWS guns
Triple 324 mm YU-7 ASW torpedoes
2 x Type 726-4 18-tube decoy rocket launchers
Aircraft carried: 1 Kamov Ka-28 'Helix' or Harbin Z-9C
Aviation facilities:
ที่สำคัญมีเจ้านี่ติดมาด้วย HN-2 long range land cruise missile
http://www.missilethreat.com/cruise/id. ... detail.asp
HN-2
Country: People's Republic of China
Alternate Name: Red Bird, YH-4
Class: S/LLCM
Target: Land
Length: 6.40 m
Diameter: 0.70 m
Wingspan: 2.50 m
Launch Weight: 1400.00 kg
Payload: Nuclear, HE, or submunitions
Propulsion: Turbofan
Range: 1800.00 km
Guidance: INS/GPS, TERCOM, radio altimeter
Status: Operational
In Service: 2002-Present
Details
The Hong Niao-2 (HN-2) is a medium-range, turbojet powered, single warhead cruise missile developed and manufactured by the People’s Republic of China. Ground-launched, ship-launched, and submarine-launched versions exist.
China is believed to have begun developing the Hong Niao family of long-range cruise missiles in 1977. The idea was to create a missile capable of carrying a nuclear warhead up to 3,000 km. Initial work was based on a design known as the X-600, which had a design range of 600 km. The X-600 used a Silkworm type body, either a Hai Ying-4 (HY-4) or Ying Ji-6 (YJ-6), with a turbojet engine attached at the rear of the missile underbody. The development program was directed by the No. 1 Research Institute, also known as the Hai Ying Electro-Mechanical Technology Academy. In the mid-1980s, all design and development work for cruise missiles was transferred to the 8359 Research Institute and the Cruise Missile Institute of China, and the manufacturing was transferred to the No. 7 Machine Building Facility.
The X-600 was first flight-tested in 1985, using a small turbojet engine specifically developed for the project. In 1988, China began developing an improved design, which was designated Hong Niao-1 (HN-1), or Red Bird-1. Two versions of the HN-1 exist: the ground-launched HN-1A and the air-launched HN-1 B. The HN-2 is a longer-range version of the HN-1 that may be based on U.S. Tomahawk cruise missile technologies recovered from crashed missiles. Three versions exist: the ground-launched HN-2A with a range of 1,800 km, the ship-launched HN-2B also with a range of 1,800 km, and the submarine-launched HN-2C with a range of 1,400 km.
The HN-2 is a significant improvement over the HN-1. It includes an improved turbofan engine based on the Russian Omsk OKB-designed TRDD-50 engine used in the SS-N-21 and AS-15 missiles, and manufactured in China after 1992. In addition, as noted above, China has incorporated technologies recovered from U.S.-made RGM/UGM-109 “Tomahawk” cruise missiles that crash landed following their extensive use in Iraq, Bosnia, Serbia, Kosovo, Afghanistan, and Sudan. These technologies include the inertial navigation system/GPS guidance system, computer hardware and software, electronics, power supplies, airframe, wings, fuel system, and small turbofan engines.
Including the tandem mounted boost motor, the HN-2 is 7.2 m long, 0.7 m in diameter, and has a launched weight of 1,400 kg. The missile has a rectangular air inlet scoop halfway between the rear of the wings and the tailplane, on the underside of the body. In addition, the wing position has been changed to a mid-body position. The missile carries a 400 kg payload, either a 20 to 90 kiloton nuclear warhead, a high explosive warhead, or submunitions. An accuracy of 5 m CEP has been reported.
The HN-2 was reportedly tested in 1995, although some sources argue that this might have been another missile. Four additional tests were reported up to October 1997, and the HN-2 is believed to have started operational evaluation in 1998. A ground-launched HN-2 was tested in August 2001. It is believed that the missile entered service in 2002. As of yet, China has not offered the HN-2 for export.(1)
น่ากลัวอย่างมากๆ เจ้าตัวนี้ติดหัวรบ 20 to 90 kiloton nuclear warhead ได้ด้วยและถ้าหากข่าวที่ว่าพม่าแอบสุ่มพัฒนาอาวุธนิวเคลียร์เป็นจริงละก็ ผมว่ากองทัพต้องเตรียมรับมือขนานใหญ่เลยทีเดียว
