Cuộc chiến của con rồng, cuộc chiến ngàn năm.

Cac ba''c goi cho em 1 cai nhe'' (tieng Anh hay tieng Viet cung duoc), ca''m on ca''c ba''c truoc
hieurusso@google.com

lo^.n )), hieurusso@gmail.com

Thế ko bác nào muốn bản tiếng Việt đã dịch ngon lành 100% à? Tôi có đây. Hôm trc đùa thôi. Free luôn. Nhưng mà đọc xong có phần thất vọng vì tác giả tả bọn Tàu ngu lắm, có lẽ cách xa sự thật hơi nhiều. Vai trò của Nga cũng rất mờ nhạt. Bắc Hàn cũng ko có võ gì ngoài biệt kích. Tên lửa hạt nhân đâu ko thấy dùng gì cả. ASEAN thì vô cùng hèn hạ (cái này chắc đúng).

Không rõ tác giả ĐR nói tới loại A7 nào của BC. Tôi chỉ tìm thấy thông tin về 2 loại A7 bomber. Loại đồ cổ này của là của Đức Quốc xã
Loại này có tên Junkers Ju290-A7 Recconaissance, dùng 37mm bắn hạ đơn giản. Loại thứ 2 là A7 của US, từng dùng trong chiến tranh VN, có tên A7-E Corsair II
http://www.intrepidmuseum.org/exhibits_a-corsair.html
Although cosmetically similar to the F-8 Crusader, the A7 Corsair II is in fact a completely distinct aircraft with a very different mission. Replacing the A-4 Skyhawk in 1967 as the Navy?Ts primary light bomber, the Corsair II flew over 90,000 combat sorties over Vietnam and saw intensive use throughout its final deployment as part of Operation Desert Storm. De-navalized versions served as subsonic tactical fighters with the Air Force and Air National Guard from 1965 to 1993
Theo tôi nghĩ thì k phải loại này, đây là loại dùng cho tầu sân bay của HK đời cổ. Bác nào có thông tin khác thì post lên tham khảo nhé!
Được KtsDzi sửa chữa / chuyển vào 16:35 ngày 02/03/2005

Còn đây là em H6 bomber, bản copy của Tu16 CCCP.
As is with the Chinese military, very little is known about advances made by the Chinese in this field. However as the case with many other countries, the Gulf war of 1991-92 had a profound impact on Chinese thinking in this field of warfare. They soon undertook a massive upgrade and re-organization plan to develop and deploy ELINT and EW systems on various platforms including ships and military aircraft. Versions of the H6 Bomber, Y8 transport and J8 II (The EJ-8 probably uses the KZ-900 pod... unfortunately not much data is available) aircraft are used to name a few. The PLAAF at present has at least two Tupolev Tu -54 EW planes obtained with the help of the Russians. These planes are planned to be part of a national C3I system. With a view of strengthening its ELINT assets the PLAAF has recently developed a HF reconnaissance system. This system is used to monitor enemy radio traffic during wartime. It can also supposedly record these HF signals. This system is said to be able to keep track of almost 500 targets and takes up the size of a small room.
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The Xi''an Aircraft Industry Corporation (XAC) Hong-6 (H-6) is the Chinese copy of the Soviet Tu-16 (NATO codename: Badger-A) twin-engine, medium-range jet bomber. It is the PLA Air Force?Ts principal medium-range ground attack platform, and supports the PLA Navy in the surface strike mission. The variant in current service include H-6D, H-6E, H-6H, H-6X, and H-6U tanker. Through extensive system upgrades, the service life of the 30-year-old H-6 is expected to continue for at least another decade.
PROGRAMME
The Tu-16 Badger medium-range bomber was developed by Tupolev Design Bureau in the late 1940s as a counter to the British Vulcan and USAF B-47 Stratojet. When the aircraft first entered service in 1953, it represented a truly remarkable achievement for the Soviet Aviation industry. The Tu-16 outperformed most of Western bombers of same age in terms of payload, speed and range. Before production of the Tu-16 stopped in 1963, a total of 1,500 examples were built in over twenty variants. The aircraft remained service with the Soviet/Russian Air Force until 1993, and continued in service with several CIS countries. It was also exported to China, Indonesia, Egypt, and Iraq.
China obtained the Tu-16 technology in the 1950s under the Treaty of Friendship, Alliance, and Mutual Assistance between China and Soviet Union. The first Chinese Tu-16 (PLAAF designation H-6) assembled from the Soviet-built kits took flight in 1959, but the indigenous H-6 using Chinese-made parts was not successful until 1968 due to technical difficulties. By the late 1980s, the PLA Air Force (PLAAF) and the PLA Naval Air Force (PLANAF) already had over 100 H-6 bombers in their inventory. The H-6 bomber also took part in China?Ts nuclear weapon programme, including the drop of China?Ts first thermonuclear (hydrogen) bomb (3,300kT) on 17 June 1967. Despite its capability to drop nuclear weapons, H-6 bombers currently in service with the PLA are only used for tactical conventional bombing missions.
The subsonic H-6 is generally regarded as obsolete by today?Ts standard. Without the sophisticated avionics and high-speed performance, the aircraft is highly vulnerable to modern air defence weapons. However, China?Ts incapability to find a suitable successor means that the PLA has to extend the service life of this thirty-year-old design for at least another decade. As well as modernising the existing H-6 fleet with updated avionics and weapon systems, the PLAAF is also building new airframes under the new generation model H-6H, which has the capability to launch stand-off attack, precision-guided weapons outside the range of enemy air defence. In ad***ion, the PLAAF and PLANAF also operate a small number of specially designed H-6s for aerial refuelling and electronic warfare purposes.
H-6D
The H-6D is the first major development variant of the H-6 family. The development began in 1975 and the aircraft entered service in 1984. The H-6D is designed to carry two YJ-6 (export designation: C-601, NATO codename: CAS-1 Kraken) anti-ship missiles to attack surface targets. The aircraft is fitted with Type 245 target acquisition/illumination radar accommodated in the enlarged under-nose radome. At the altitude of 9,000m, the radar can detect a surface target of RCS 7,500 square metre 150km away. To perform long-range counter maritime operations, the H-6D is also fitted with improved avionics, including a new fire-control system that can be used for automatic navigation, automatic missile attack and semi-automatic level bombing.
The semi-active radar-homing YJ-6 was derived from the HY-2 ship-/land-based anti-ship missile. It is fitted with a 500kg high-explosive warhead, and can attack surface target 120km away at a speed of Mach 0.8. Two missiles are carried by the under-wing hardpoints. All 23mm cannons on the original design were removed, so the aircraft relies entirely on onboard electronic warfare (EW) suite and escort fighter aircraft for protection. The internal bomb bay is retained for conventional level bombing mission.
H-6E
Early variant H-6A bombers in the PLAAF and PLANAF have been replaced by the improved second-generation H-6E, which was introduced in the late 1980s. The H-6E is distinguished from early variants of the H-6 by its light-grey low visibility colour scheme and the removal of the 23mm nose cannon. On some H-6E bombers the dorsal twin-23mm cannon turret is also removed. Inside the aircraft is equipped with an integrated navigation system comprising three navigation methods?"inertial, global position system (GPS), and a Doppler navigation radar. The original manually operated bombing sight is also replaced by an automatic fire-control system, which enables the aircraft to perform long-range air-interdiction and offensive counter maritime missions at low-altitude in all-weather, day/night con***ions.
Despite these upgrades, like its ancestor the H-6E is only capable of conventional level bombing mission. Although this may pose certain threats to an individual surface ship, the possibility of the bomber *****rvive enemy?Ts inland air defence system comprising surface-to-air missiles (SAMs), ground-based radar, and airborne early warning (AEW) aircraft is very low.
H-6H
The H-6H bomber was developed in the 1990s to meet the PLAAF?Ts requirement for a new aerial platform that can launch ?~stand-off?T land-attack weapons outside the range of enemy?Ts air defence system, thus increasing the survivability of the bomber in modern air combat. The development of the H-6H began in January 1995, and the aircraft first flew in December 1998. The first successful missile fire test took place in November 2002. Currently two prototypes are undertaking various flight and system tests before the design can be finalised for batch production.
Based on the design of the H-6D naval anti-ship missile carrier bomber, the H-6H carries two YJ-63 (also known as KD-63) LACMs on its under-wing hardpoints. The YJ-63 is a land-attack cruise missile (LACM) developed from the HY-4 (XW-41) anti-ship cruise missile. Powered by a small turbojet, the YJ-63 delivers a 500kg HE warhead over a distance of 200km at subsonic speed. While guided by inertial/GPS midcourse homing coupled with TV-command terminal guidance, the missile also receives target information via the bomber?Ts datalink antenna accommodated in the under-belly fairing behind the bomb bay doors. Like the H-6D, the H-6E is not equipped with any 23mm cannon.
H-6X
The H-6X is the new generation naval anti-ship missile bomber developed between 2001 and 2004 to replace the H-6D in service with the PLANAF. The H-6X carries four YJ-83 (C-803) anti-ship cruise missiles on its under-wing hardpoints. Powered by a turbojet engine, the semi-active radar-homing YJ-83 is said to have a maximum range of 250km and final approach speed of Mach 1.2. An infrared seeker might be fitted to give the missile an all-weather, day/night strike capability. The introduction of the H-6X will greatly increase the capability of the PLANAF to conduct offensive counter maritime operations.
DEPLOYMENT
Currently around 120 aircraft are deployed by the PLAAF 8th Air Division (Hengyang, Hunan Province), 10th Air Division (Anqing, Anhui Province) and 36th Air Division (Wugong, Shaanxi). The PLANAF also deploys some H-6 bombers.
DESIGN
The H-6 has mid-mounted, swept-back wings with blunt tips, fences on top of the wings, and landing gear pods extend beyond the wings trailing edges. Two WP-8 turbofans are mounted in wing roots which extend beyond the leading and trailing edges of the wing root. The engines have a pair of round air intakes. The fuselage is long, slender, and bulging where the engines are mounted and tapered to the tail. The aircraft has a round, glassed-in nose and a stepped ****pit. The tail is swept-back, tapered fin and flats with blunt tips and a tail gunner compartment.
The aircraft has a under-chin radome to accommodate the navigation radar. There are five crewmembers onboard: Two pilots seated in the central ****pit, each with an independent flight control; a navigator and a bombing aimer seated in the glassed-in nose compartment, and a rail gunner seated in the tail compartment. All crews are equipped with eject seats (two upwards, two downwards), but the eject seats are reported to have poor survivability.
POWERPLANT
The aircraft is powered by two Xi''an (XAE) WP-8 (Mikulin AM-3M-500) turbojets, with a maximum thrust of 20,944 lb (93.16 kN) dry each.
WEAPONS
Up to 9000kg (normally 3,000kg) of disposable stores are carried in a lower-fuselage weapon bay capable of accepting nuclear and/or 250/500/1,500/3,000 kg high-explosive (HE) free-fall bombs.
Early variant H-6 also has seven 23mm cannons, with one single-barrel mounted on the starboard side of the glass-nose, three twin-barrels mounted in defensive turrets located on the back and belly of the fuselage and tail. These cannons are controlled by optical sight/fire-control radar. Later variants have all of these cannons removed.
Later variants also have two or four hardpoints under the wings to carry air-to-surface missiles.
SPECIFICATIONS
Crew: 5
Length: 34.8m
Wingspan: 34.2m
Hight: 9.85m
Normal take-off weight: 72,000kg
Maximum take-off weight: 75,800kg
Normal weapon Load: 3,000kg
Maximum weapon load: 9,000kg
Internal fuel: 33,000kg
Maximum speed: 1,014km/h;
Cruising speed: Mach 0.75 (786km/h)
Maximum range: 6,000km
Combat radius: 1,800km
Service ceiling: 13,100m
Date Last Updated: 1 January 2005

Tiếp tục là em J8 (không phải S8) được dùng hộ tống đàn H6. J8 là bản upgrade của J7 - phiên bản copy của Mig 21. Tôi không rõ về rada của J8, nhưng các tính năng khác của nó chỉ tương đương Mig 21 bis. Chi tiết các bác xem tạm = tiếng Anh nhé:
J-8 Interceptor Fighter Aircraft
The Shenyang Jian-8 (J-8, also known as F-8 in its export form, NATO code-name: Finback-A) is the single-seat, twin-engine interceptor fighter aircraft developed by Shenyang Aircraft Industry Corporation (SAC). The basic variant J-8 is a day fighter developed in the 1960s/70s. The J-8A (also known as J-8I) is an improved all-weather fighter fitted with a ranging radar and entered service in the early 1980s. Both aircraft are still in service with the PLAAF and the PLA Naval Air Corps for homeland defence roles, though their capabilities are limited by their poor performance.
PROGRAMME
In response to the competitions between the U.S. and the Soviet Union in the early 1960s to develop the new-generation high-altitude, high-speed bombers and spy planes, the Chinese leaders decided to develop a new type of fighter aircraft with similar performance as a counter to the threats. Careful studies on different design proposals has led the PLA to select the J-8 fighter proposed by the 601 Institute (Shenyang) and the J-9 fighter proposed by the 611 Institute (Chengdu).
Compared to the J-9, which is a wholly new design with solid nose and lateral air inlets, the J-8?Ts design is much less radical. The basic concept of the J-8 programme is to enlarge the fuselage of the MiG-21/J-7 Fishbed fighter to accommodate two engines instead of one, with changes on the rest parts of the aircraft minimised. This is apparently more practical considering the capability of the Chinese aviation industry at the time. Not surprisingly, the J-9 project was later cancelled due to technical difficulties.
The development of the J-8 fighter began in 1964. Unconfirmed reports claim that the J-8 may have borrowed some designs from the Mikoyan-Gurevich Ye-152A experimental aeroplane about which the Chinese had received limited data in the late 1950s. The programme developed at a very slow pace partially due to the interruptions of the ?~culture revolution?T in the 1960s/70s. The maiden flight of the aircraft did not take place until 5 July 1976, and the first two prototypes only undertook limited flight tests. The batch production of the J-8 was finally authorised by the Ministry of Aeronautics in July 1979, some 25 years after the programme began.
The basic variant J-8 is only a day fighter with no fire control radar for night combat. Therefore the SAC revealed the J-8A (also known as J-8I) in September 1984. The J-8A is added with a Sichuan Changhong SR-4 fire-control radar accommodated in the aircraft?Ts nose inlet centre-body. Three J-8A prototypes were built, one being lost in a fire accident before making any flights, so it was the second prototype that recorded the variant''s first flight on 24 April 1981.
The J-8A was authorised for production on 27 July 1985, but only around 130 examples were built before production was halted in 1992. Most of these aircraft were delivered to the PLAAF and the PLA Naval Aviation Corps, with about 10~20 exported to Iraq in the 1980s. Some J-8As were upgraded with new fire-control radar and avionics in the 1990s and re-designated as J-8E. In ad***ion, the PLAAF has also converted some of its basic variant J-8 for air reconnaissance roles. These aircraft are designated as JianZhen-8 (JZ-8).
VARIANTS
J-8: The basic variant day fighter.
J-8A: Upgraded all-weather fighter.
JZ-8: (Jianji Zhencha, or Jian Zhen = Fighter Reconnaissance) Tactical reconnaissance aircraft converted from the basic variant J-8, equipped with two optical/IR camera pods carried under the wings.
J-8E: This designation is used by the J-8A which have received mid-life upgrade including a new fire-control radar.
DEPLOYMENT
PLA Air Force and PLA Naval Air Corps.
DESIGN
The J-8 is rather straightforward magnified version of the Chengdu J-7 (MiG-21) to accommodate two engines. The aircraft has a pair of large delta wings and two stabilising fins located under the engine nozzles. The J-8 has a front-hinged ****pit canopy, and the J-8A?Ts canopy is back-hinged. The aircraft is powered by two WP-7A turbojets to secure Mach 2 performance. The engines are aspirated through a single large nose inlet with a translating centre-body, which accommodates the fire-control radar on the J-8A.
The frame layout of the J-8 is obsolete, causing poor aerodynamic performance. The aircraft was designed to simple tasks of intercepting strategic bombers and spy planes flying on high altitude at supersonic speed, and is vulnerable in the much more complicated modern air combat environment.
WEAPONS
The fixed armament includes a twin-barrel 23 mm Type 23-III cannon. Five stores stations (four under wings and on uner fuselage) can carry up to 4,500 kg weapons.
The aircraft can carry 4 PL-2 or PL-5B short-range IR-homing AAMs. Ground attack weapons include 500, 250, 100, 50 kg free-fall iron bombs, or multiple launchers each carrying eighteen 57mm or seven 90mm unguided rockets.
RADAR
The early basic variant J-8 has no radar and can only combat in day time. The J-8A is fitted with SL-8 optical sight, Sichuan Changhong SR-4 ranging radar, and Type 903 rear warning receiver (RWR). The updated J-8E may be fitted with updated IFF, RWR, HUD and fire-control radar.
POWERPLANT
The J-8 is powered by two Wopen-7A (WP-7A) turbojets (A Chinese-built version of the Tumanskii R-11F-300).
SPECIFICATIONS
Crew: 1
Dimentions: Wingspan 9.34 m; Length 21.52 m; Height 5.41 m
Weight: Empty 9,285 kg; Normal take-off 13,850 kg; Max take-off 16,580 kg; fuel 4,600 kg; Weapon payload 4,500 kg
Powerplant: Two Liyang (LMC) Wopen-7A turbojets each rated at 43.15 kN dry and 58.8 kN (6,000 kg) with afterburning
Speed: Maximum 2,332 km/h (Mach 2.2); cruising 850 km/h
Range: Ferry range 2,000 km; combat radius 800 km
Service Ceiling: 20,800 m
Maximum Climb Rate: 163 m/s (sea level)
+G Limit: 4
Stores Stations: Five, one under the fuselage and four under the wings, up to 4,500 kg

Đây là em JH7 của Hải quân Khựa, có trang bị khá mạnh để tấn công mặt đất.JH-7 (FBC-1 Flying Leopard) Fighter-Bomber
The JianHong-7 (JH-7, also known as FBC-1 in its export form) is the two-seater, twin-engine fighter-bomber aircraft designed by 603 Aircraft Design Institute and built by Xi?Tan Aircraft Industry Corporation (XAC). A small number (16~20) of this aircraft has been in service with the PLA Naval Air Corps for operational test and evaluation since the mid-1990s. The improved variant JH-7A first flew in 2001 and reportedly entered the service in 2004.
PROGRAMME
In the early 1970s, the Chinese Ministry of Aeronautics (MOA) was requested by the PLA to develop a new generation lightweight tactic bomber to replace its obsolete H-5/IL-28 Beagle bomber and Q-5 Fantan ground attack aircraft fleets. The aircraft, which should be able to attack surface targets in all weather, both day and night con***ions, was to be built in two variants for the PLAAF and Naval Air Corps respectively on the basis of one airframe design. Performance requirements included a ferry range of over 2,800 km, a combat radius of over 800 km, a maximum speed of Mach 1.5, a standard weapon payload of 3 tonnes and a maximum weapon payload of 5 tonnes. Shenyang, Nanchang and Xi?Tan were competing to offer their designs, and the PLA finally chose the Xi?Tan Hong-7 (H-7) two-seater, twin-engine bomber powered by the British Rolls-Royce Spey RB.168 Mk 202 turbofan engines. The development began in 1977.
However, the ill-fated H-7 project did not go well from the start. The PLA Navy asked for an aerial platform to launch its YJ-8 (C-801) anti-ship missile. While the PLAAF''s demands were much more complicated -- the new bomber should be capable of high-speed, low-altitude penetration missions in night con***ion with extensive electronic countermeasures (ECM) and terrain following abilities. The PLAAF also insisted the two pilots should sit side-by-side in the ****pit instead of the tandem ****pit layout required by the navy. As a result, the development of the H-7 was seriously delayed.
By 1980 it became clear that the XAC could not afford developing two variants with so much difference within one programme. The air force version H-7 was temporarily postponed while the navy variant headed for the development stage. Soon the development work slowed down again because the economic development was given higher priority. The programme did not resume full speed until 1982, when the PLA leaders were impressed by the Argentinean Air Force using air-launched anti-ship missiles to sink British warships during the Farklands War. Later the aircraft was re-designated as JianHong-7 (JH-7) fighter-bomber.
By 1987 six prototypes had been built, and the aircraft?Ts maiden flight took place on 14 December 1988. However, the development could not be finalised until 1998 due to poor reliability of its avionics and various other problems. One prototype and two test pilots were lost during a crash caused by engine failure. The first successful test launch of the YJ-8K anti-ship missile from the JH-7 took place in 1998.
Meanwhile around 12 aircraft are deployed by the PLA Naval Air Corps for operational test and evaluation (OT&E) phase, which is known as production finalisation, and they are not considered fully operational. Several of the aircraft over flew Beijing during the PRC''s 50th anniversary on 1 October 1999.
In response to the problems merged during the trial service, and other design drawbacks, the XAC began to develop the improved variant JH-7A, which features more advanced avionics and weapon suites based on both Russian and domestic technologies including the new multi-mode JL-10A PD fire-control radar, revised fly-by-wire (FBW), and 11 stores stations to carry guided ground attack weapons. Other modifications include removing the wing fences, replacing the single underbelly fin with two fins, and a new one-piece windshield.
VARIANTS
JH-7: Initial production variant, with 16~18 examples built, inlcuding 5 prototypes.
JH-7A: Improved variant.
DEPLOYMENT
12 aircraft are being deployed by the PLA Naval Air Corps 6th Air Division based at Dachang AFB near Shanghai.
DESIGN
The JH-7 is a two-seater, twin-engine all-weather supersonic fighter-bomber aircraft, which is similar in configurations and roles to the European Tornado GR3 ground attack aircraft and the Russian Su-24 Fencer fighter-bomber aircraft. However, the aircraft?Ts performance is constrained by its underpowered WS-9/Spey Mk 202 turbofan engines. With a maximum take-off weight of 27 tonnes, the JH-7 has a maximum weapon load of only 5 tonnes, much less than that of those Russian- or Western-made combat aircraft in the same class of weight.
The JH-7 has high-mounted wings with compound sweepback, dog tooth leading; twin turbofans, with lateral air intakes; all swept tail surface, comprising large main fin, single small ventral fin and low set all moving tail plane; small over-wing fence at approximately two third span. Quarter chord sweep angles approximately 45 degrees on wings and fins, 55 degrees on tail plane. The JH-7 has a tandem two-seat ****pit, with the rear seat slightly higher than the front seat to give the weapon operator a better filed of view. Each seat has its own back-hinged canopy. The ****pit and internal fuel tank are protected by armours.
AVIONICS
The JH-7 is fitted with a Type 232H Eagle Eye multi-function PD fire-control radar, while the JH-7A has a more capable JL-10A PD fire-control radar with better reliability and longer detect range. The front-seat pilot ****pit is fitted with a HK-13-03G head-up display (HUD), two black-white multi-function displays (MFDs) and one colour MFD. The fire-control system for the YJ-8K anti-ship missile is fitted in the rear-seat (weapon operator) ****pit. Combat data is processed by the mission computer through the Mil1553B digital databus.
Flight control systems include the KF-1 digital fly-by-wire (FBW), 8145 air-data computer, WG-5A radio altimeter, HG-563GB INS/GPS navigation system, the Type 210 Doppler navigation system, HZX-1B stabilising system, and microwave landing assistance system.
Communications systems include HF, UHF, VHF, Type 483D data transmission/TAKAN system.
COUNTERMEASURES
Electronic countermeasures (ECM) suite includes the Type 605B IFF; KJ-8602/RW-1045 RWR; Type 960-2 or KG-8605 (JH-7A) internal radar noise jammer; KZ-8608 ELINT; GT-1 chaff/flare dispenser.
The JH-7 can also carries an indigenous Blue Sky low altitude navigational pod under wings. The aircraft is also seen carrying two weapon designation pods under the air inlets. One is believed to be a Chinese copy of the Russian design which can collect the enemy radar emissions to guide the YJ-91/Kh-31P anti-radiation missile. The other one is possibly a laser designation pod for the laser-guided bombs.
WEAPONS
The JH-7 is equipped with a two-barrel 23 mm Type 23-III (a copy of the Gryazev-Shipunov GSh-23L) cannon with 300 rounds in a ventral installation. There are two (JH-7A has three) stores pylons under each wing, plus rail for the PL-5 close-range IR-guided air-to-air missile (AAM) at each wingtip.
For a typical anti-ship mission, the aircraft carries four YJ-8K (C-801K) and YJ-82K (C-802K) sea-skimming anti-ship missiles (ASMs), or two missiles plus two 600 kg drop tanks, and two PL-5 AAMs. The JH-7A can carry two YJ-91 (Chinese copy of the Kh-31P) anti-radiation missiles (ARMs) for suppress of enemy air defence (SEAD) mission.
For ground attack missions, the JH-7 can carry free-fall bombs and unguided rocket launchers. The JH-7A can also carry laser-guided bombs for precision strike.
POWERPLANT
The JH-7 is powered by two British-made Rolls-Royce Spey RB.168 Mk 202 turbofan engines, each rated at 5,556 kg dry and 10,000 kg with afterburning.
Rolls-Royce has consented to allow Xi''an Aviation Engine Company (XAE) to build the Spey Mk 202 turbofan under license, but the programme was seriously delayed due to technical problems. As a result, XAC had to imported from the UK some second-hand Spey Mk 202 stripped from the retired RAF F-4 Phantom fighters.
The latest reports indicated that XAE has successfully tested the WoShan-9 (WS-9), the Chinese copy of the Spey Mk 202. The engine will be used to power the new JH-7A due to enter the service shortly.
SPECIFICATIONS
Crew: Two (1 pilot and 1 weapon operator)
Wingspan: 12.8 m
Length: 21.00 m
Height: 6.22 m
Maximum take-off weight: 27,500 kg
Internal fuel: 6,540 kg
Drop tanks: One 1,000 kg + two 600 kg; or three 1,000 kg
Maximum speed: Mach 1.69 (at 11,000 m)
Service ceiling: 16,000 m
Range: Ferry range 3,650 km, combat radius 1,650 km
Date Last Updated: 21 February 2004

Một vài hình ảnh của JH7, định up lên thì nhận được thông báo lỗi thế này:
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Vậy là sao, các bác giúp em với. Hoặc bác nào k bị lỗi thì cho em địa chỉ mail, em gửi ảnh nhờ upload vậy!
kts.dzi@fpt.vn
Được KtsDzi sửa chữa / chuyển vào 18:01 ngày 02/03/2005

Vậy bác gửi cho em một bản được không? Cám ơn bác trước nhiều lém.
hiengiabala@yahoo.com

Bản pdf được upload lên Yahoo Group quá tốt, không hiểu sao Excocet phải type cho mất công. Có thể Copy & Paste được mà.