Data on the Chinese varient of the Iranian missile clone
CSS-N-4 'Sardine' (YJ-1/-12/-82 and C-801) and CSSC-8 'Saccade' (YJ-2/-21/-22/-83 and C-802/803)
Type
Short-range, ground-, air-, submarine- and ship-launched, solid propellant or turbojet-powered, single warhead, air-to-surface and surface-to-surface missiles.
Development
A second variant, YJ-2, completed development in 1993 (C-802A for the ground- or ship-launched export version and C-802K for the air-launched version) with the solid-propellant sustainer motor being replaced by a turbojet engine to give longer range. It is believed that this version has the NATO designator CSSC-8 'Saccade', which is a coastal defence designator. Alternate reports suggest the NATO designator is CSS-N-8 'Saccade', which is a ship-launched designator, and it is possible that an air-launched designator (CAS-8 'Saccade') was also used. YJ-2 started development in 1985 and was first tested in 1990. Small turbojet technology in China was initially developed from recovered US BQM-34 Firebee drones, but later supplemented by auxiliary power units imported for use on civil aircraft programmes. YJ-2 missiles are fitted to 'Song' and 'Han' class submarinies, 'Luhai' and 'Luhu' class destroyers, 'Jiangwei 1 and 2', 'Jianghu 3 and 4' and type 054 class frigates, fired from above deck launchers. The YJ-83 or YJ-8-3 improved YJ-2 version started development in 1992. This version has the export designator C-803. It is reported that the YJ-83 version has the capability to cruise at supersonic speed, and has an extended maximum range. This version can be ground- and ship-launched, air-launched, and the encapsulated version can be launched through standard 533 mm torpedo tubes. YJ-2 or YJ-83 missiles are expected to be fitted to the new type 093 SSN and the type 041 Yuan class submarines.YJ-2 and YJ-83 missiles are believed to have been cleared for carriage on Tu-16 'Badger' H-6M, Su-27, Su-30MKK, Q-5 and JH-7 aircraft and the CHAIC Z-8 helicopter with two missiles carried by each, although the JH-7 may be able to carry four missiles. It is believed that YJ-2 and YJ-83 missiles will be retrofitted to Chinese ships in place of YJ-1 missiles. The first 'Luhu' (Type 052) class destroyer came out of refit in 2002 with 16 cylindrical missile canisters in two octuple groups aft of the funnel, and these are believed to house YJ-83 missiles. An unconfirmed report in April 2003 indicated that an imaging IR seeker was being developed for the YJ-83 missile, to provide a land attack capability. 'Huangfen' fast attack craft, known as 'Hudong', have been exported to Iran for use with both YJ-1 and YJ-2 missiles, and it is reported that YJ-2 missiles are being built in Iran with the name 'Tondar'. Reports in 1994 indicated that an increased range YJ-2 version was also in development, designated YJ-21. A second development, YJ-22, was reported in 1997, adding wings to the YJ-21 design to increase the range to 400 km.
Description
YJ-1 is similar in appearance to the French MM 38 Exocet, but the Chinese missile is heavier. YJ-1 has four clipped delta-wings at mid-body and four small clipped-tip triangular moving control fins at the rear. The overall length including the tandem-mounted booster motor is 5.81 m for the ground- and ship-launched versions, the body diameter is 0.36 m, the wing span is 1.18 m and the launch weight 815 kg. The tandem-mounted solid-propellant boost motor weighs 160 kg and is jettisoned after use. The air-launched version does not have a tandem boost motor, having a length of 4.65 m, and a weight of 655 kg. Mid-course guidance is inertial, with a monopulse active radar (probably X-band) in the terminal phase. The cruise altitude is believed to be around 20 m, followed in the terminal phase by a descent to between 5 and 7 m, both being controlled by a radio altimeter. YJ-1 has a high explosive warhead with a weight of 165 kg. The missile flies at around M0.85. YJ-1 is reported to have a minimum range of 8 km and a maximum range of 40 km when ground- or ship-launched, and a maximum range of 50 km when air-launched from medium altitude (30,000 ft).
YJ-2 has an air inlet scoop beneath the missile body between the central wings to serve the turbojet engine that has replaced the solid-propellant sustainer motor of the earlier YJ-1 version. The engine is a Chinese-built version similar to the Microturbo TRI-60-2. The missile has a cruise speed of M0.85, the mid-course cruise can be set at either 30 or 20 m and the terminal altitude at either 7 or 5 m. Guidance in mid-course is inertial with a monopulse active radar operating at 10 to 12 GHz (X-band). YJ-2 is longer at 6.39 m for the ground- and ship-launched version, but has a reduced launch weight of 715 kg. The tandem boost motor weighs 160 kg and is jettisoned after burnout. The air-launched version, without a boost motor assembly, has a length of 5.3 m and a launch weight of 555 kg. It is reported that YJ-2 has a maximum range of 120 km when ship or ground launched and 130 km when air-launched from medium altitude (30,000 ft), and a minimum range of 15 km. The warhead remains the same as for YJ-1.
YJ-83 (or YJ-8-3) has a turbojet engine, but can cruise at supersonic speed. This missile is similar in external appearance to the YJ-2, and was seen as an interim solution until ramjet-powered missiles had been developed. However, the versatility of the YJ-1/YJ-2/YJ-83 family probably means that they will remain in use for many years. YJ-83 can be launched from submarine torpedo tubes, and is fitted inside a launch capsule, which is ejected after broaching the water. The missile can also be carried by aircraft, and launched from ships or coastal defence TEL. The ground- and ship-launched versions have a maximum range of 160 km, and the air-launched version a maximum range of 250 km. These longer ranges are achieved by inserting a subsonic high level (10 km) cruise phase, but the terminal phase can be flown at supersonic speed, reported to be between M1.3 and M1.5. This version has a datalink, which can be used to update the target co-ordinates during flight, alter the switch on timing for the active/passive terminal radar seeker, or re-allocate targets in the terminal phase. The YJ-83 can cruise at between 10 and 30 m altitude, reducing to 5 m in the terminal phase. It is believed that the first ship-launched YJ-83 missiles have been fitted to the 'Luhu' class destroyers, where they are in cylindrical canisters, and it is possible that the same canisters will be used for ground-launched TEL.
A typical YJ-1 or YJ-2 coastal defence battery has a radar-command truck, a power supply vehicle and four Transporter-Erector-Launcher (TEL) vehicles. The YJ-1 TEL vehicles carry two missiles in their canisters, and can launch against targets in a 160º sector. The YJ-2 TEL vehicles carry three missiles in their canisters, and these wheeled vehicles are converted trucks with three axles.
Specifications
YJ-2/-83 (C-802/-803)
Length: 6.39 m (ground/ship), 5.3 m (air)
Body diameter: 0.36 m
Launch weight: 715 kg (ground/ship), 555 kg (air)
Payload: Single warhead; 165 kg
Warhead: HE
Guidance: Inertial and active radar (YJ-2), inertial, command updates, active/passive radar (YJ-83)
Propulsion: Solid-propellant boost and turbojet
Range: 120 km (YJ-2 ground/ship), 130 km (YJ-2 air), 180 km (YJ-21 air), 160 km (YJ-83 ground/ship), 250 km (YJ-83 air)
Accuracy: n/k
Status
YJ-1 is in production and the ground- and ship-launched versions entered service around 1984 with the Chinese armed forces. The air-launched version is believed to have entered service in 1989. A reported purchase of YJ-1 (C-801 export version) by Thailand in 1990, for 50 missiles to arm their 'Jianghu 4' class frigates, was the first known export of YJ-1. Further exports could have been made to Iran, North Korea and Yemen for use as coastal defence weapons from fixed sites or mobile launchers. Iran has fitted YJ-1 missiles to F-4 Phantom aircraft and trials launches were made in 1997. An unconfirmed report suggests Iran is building YJ-1 (C-801A and C-801K) missiles under the project name 'Karus'. About 500 YJ-1 and YJ-82 missiles are thought to be in service in China. A modified version, known in China as YJ-12, was reported to be in development in 1996.
YJ-2 was first tested in 1990, and could have entered service with the Chinese Navy in 1994. YJ-21 may have entered service in 1998, and there were two test launches made in May and July 2001. Reports in 1995 stated that 100 YJ-2 missiles had been ordered by Iran, with test launches from ground sites reported in early 1996 and fitment to 'Hudong' fast attack craft. Up to 10 'Hudong' PCFG (Patrol Craft Fast-Guided) have been delivered to Iran, each capable of carrying four YJ-2 missiles. Later unconfirmed reports suggest that Iran may be manufacturing YJ-2 missiles under licence, with the project name 'Tondar'. Iran is known to have developed a Tolloue 4 turbojet engine, similar to the Chinese version of the Microturbo TRI-60-2 used in the C-802 missile. Pakistan ordered YJ-2 missiles in 1997 to fit to their Jalalat 2 FACs, with four missiles per boat. The first YJ-83 version (or YJ-8-3) is believed to have entered service in 1998, and was displayed in Beijing in October 1999. YJ-83 missiles were launched from JH-7 aircraft in July and November 2002, demonstrating a maximum range of 250 km. An unconfirmed report in August 2002 suggested that YJ-83 missiles would be fitted to Pakistani 'Khalid' class (Agosta 90B) submarines. In 2005 Indonesia was reported to have ordered C-802 missiles for fitting to a new FAC.