from Wikipedia
The YJ-7 (Chinese: 鹰击-7; pinyin: yingji-7; lit. 'Eagle Strike 7') is a Chinese subsonic anti-ship missile. It is manufactured by the Third Academy of the China Aerospace Science and Industry Corporation (CASIC).[3] The export version of the YJ-7 is the C-701.[1]
Key Information
History
[edit]The radar-guided C-701 was displayed by the China Precision Machinery Import-Export Corporation (CPMIEC) at the 2004 China International Aviation & Aerospace Exhibition.[4] Although the missile was developed by the China Aerospace Science and Industry Corporation, Iran's Aerospace Industries Organisation (AIO) claimed presented the missile as a national program.[5]
In April 2006, it was reported that radar-guided C-701s were fired during Iranian military exercises.[4]
Variants
[edit]Operators
[edit]
Current operators
[edit]- Armed Forces of the Islamic Republic of Iran: C-701, Kowsar (patrol boats,[7] shore batteries.[8])
- People's Liberation Army Navy: YJ-7 (Harbin Z-8 and Z-9C helicopters)[9]
See also
[edit]References
[edit]- ^ a b c d e Gormley et al.: page 16
- ^ a b Cordesman and Lin: page 28
- ^ a b Gormley et al.: page 18
- ^ a b China Missile Chronology: section "10 April, 2006"
- ^ Hewson, Robert (17 November 2004). "China aids Iran's tactical missile programme". Jane's Defence Weekly.
- ^ Cordesman and Lin: page 41
- ^ Cordesman and Lin: page 30
- ^ Cordesman and Lin: page 29
- ^ Gormley et al.: page 58
- Bibliography
- "China Missile Chronology" (PDF). Nuclear Threat Initiative. 8 June 2012. Retrieved 1 February 2021.
- Cordesman, Anthony H.; Lin, Aaron (February 2015). The Iranian Sea-Air-Missile Threat to Gulf Shipping (PDF). Center for Strategic and International Studies. ISBN 978-1-4422-4077-3.
- Gormley, Dennis M.; Erickson, Andrew S.; Yuan, Jingdong (2014). A Low-Visibility Force Multiplier: Assessing China's Cruise Missile Ambitions (PDF) (Report). Washington, D.C.: National Defense University Press.
from Grokipedia
Development
Origins and Initial Design
The YJ-7 anti-ship missile originated in the late 1980s amid China's efforts to indigenously develop lightweight, cost-effective weapons for smaller naval and air platforms, including fighter aircraft, helicopters, and patrol boats, to enhance tactical anti-surface strike capabilities without relying on larger, more expensive systems. The project addressed gaps in the People's Liberation Army Navy's arsenal for precision engagements against coastal and littoral targets, prioritizing modularity and affordability over extended range or supersonic performance. Development was led by the Third Academy of the China Aerospace Science and Industry Corporation (CASIC), a state-owned entity established in 1961 and specialized in cruise missile research, design, and production.[7][8] Initial design work emphasized a compact, subsonic configuration powered by a solid-fuel rocket motor, enabling launches from constrained platforms while maintaining structural simplicity for mass production. The baseline concept incorporated interchangeable guidance options—primarily active radar homing for autonomous terminal acquisition, with electro-optical and television variants for operator-in-the-loop control in scenarios requiring visual discrimination amid decoys or civilian shipping. This approach reflected pragmatic engineering trade-offs, balancing seeker accuracy against the limitations of subsonic flight profiles vulnerable to countermeasures, and positioned the YJ-7 as a counterpart to systems like the U.S. AGM-65 Maverick in scale and role.[9][10] The export-oriented C-701 variant, managed through the China Precision Machinery Import-Export Corporation (CPMIEC), marked the design's public debut at the Zhuhai International Aviation and Aerospace Exhibition in November 1998, where it was showcased in air-launched and surface configurations to attract foreign interest. Subsequent flight testing of prototypes began around 2002, validating core aerodynamic and propulsion elements prior to serial production and integration into Chinese service.[11][12]Production and Manufacturer Details
The YJ-7 anti-ship missile is manufactured by the Third Academy of the China Aerospace Science and Industry Corporation (CASIC), known alternatively as the China Haiying Electro-Mechanical Technology Academy (CHETA).[13] This state-owned entity functions as CASIC's principal research, development, and production hub for anti-ship cruise missiles.[13][1] Established in 1961, the Third Academy has designed and developed over 20 types of cruise missiles, contributing to China's indigenous missile capabilities since the early post-liberation era.[1] Production of the YJ-7 occurs within dedicated facilities under CASIC, which has publicly showcased a complete anti-ship missile assembly line capable of handling the lightweight YJ-7/C-701 series for both domestic and export needs.[14] While specific production volumes and timelines for the YJ-7 remain classified, the missile's integration into People's Liberation Army platforms indicates serial manufacturing scaled to operational requirements, with export variants marketed through the China Precision Machinery Import-Export Corporation (CPMIEC).[11] The Third Academy's role underscores CASIC's centralized control over precision-guided munitions, prioritizing modular designs for diverse launch platforms.[13]Design and Technical Features
Physical and Performance Specifications
The YJ-7 missile measures 2.5 meters in length and 0.18 meters in diameter.[15] [11] It has a launch weight of approximately 117 kg.[7]| Specification | Value |
|---|---|
| Warhead | 29-30.5 kg semi-armor-piercing high explosive[7][15] |
| Engine | Solid rocket motor[15] |
| Maximum speed | Mach 0.8 (subsonic)[15] |
| Operational range | 25 km[7][15] |
Guidance, Propulsion, and Warhead
The YJ-7 employs terminal guidance via seeker heads that enable precision targeting of surface vessels, with options including electro-optical systems (television or infrared imaging) for daylight or clear-weather operations and active radar homing (millimeter-wave) for all-weather capability. Export variants of the missile, such as the C-701T, utilize electro-optical seekers, while the C-701 AR features active radar guidance; the domestic YJ-7 incorporates comparable technologies tailored for People's Liberation Army requirements.[16][9] Propulsion is provided by a solid-fuel rocket motor, which propels the missile to subsonic speeds reaching Mach 0.8 at low altitudes of 15-20 meters to evade detection. This unpowered boost-glide profile suits short-range engagements, yielding effective ranges of 15-25 kilometers from air, surface, or coastal launches, with no sustained turbojet required due to the lightweight design.[15] The warhead is a 30 kg high-explosive semi-armor-piercing type equipped with a time-delay fuze, optimized to penetrate hulls of small to medium displacement ships (up to 1,000-3,000 tons) before detonating internally for maximum structural damage. This payload balances the missile's 117 kg total mass, prioritizing lethality against fast attack craft over larger warships.[2][17]Variants
Domestic YJ-7
The YJ-7 represents the indigenous variant of the lightweight, subsonic anti-ship cruise missile (ASCM) developed by the Third Academy of the China Aerospace Science and Industry Corporation (CASIC) exclusively for integration into People's Liberation Army (PLA) platforms. Designed for precision strikes against surface vessels in littoral environments, it supports anti-access/area-denial (A2/AD) strategies through its compatibility with compact launch systems on small attack craft, helicopters, and mobile coastal batteries. Guidance employs electro-optical or active radar seekers for terminal homing, with electro-optical variants emphasizing the domestic configuration's focus on over-the-horizon targeting in contested waters.[1][18] Key technical specifications include a total mass of approximately 117 kg, a high-explosive semi-armor-piercing warhead weighing 30.5 kg, and a solid rocket motor providing subsonic propulsion (Mach 0.8–0.9). The missile achieves a maximum effective range of 25 km, with a length of about 2.1 m and diameter of 0.18 m, enabling multiple-unit salvos from constrained platforms without compromising stability.[1][18]| Parameter | Specification |
|---|---|
| Mass | 117 kg |
| Warhead | 30.5 kg HE semi-AP |
| Range | 25 km |
| Speed | Subsonic (Mach 0.8–0.9) |
| Guidance | Electro-optical / active radar |
| Propulsion | Solid rocket |
| Platforms | Air, surface, ground |