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Silkworm (missile)
View on WikipediaThe SY (Chinese: 上游; pinyin: Shàngyóu; lit. 'Upstream'), and HY (Chinese: 海鹰; pinyin: Hǎiyīng; lit. 'Sea Eagle') series were early anti-ship cruise missiles (ASCM) developed by the People's Republic of China from the Soviet P-15 Termit missile. They entered service in the late 1960s[2] and remained the main ASCMs deployed by the People's Liberation Army Navy through the 1980s. The missiles were used by the PRC and export customers to develop land-attack missiles.[3]
Key Information
The name Silkworm is popularly used for the entire SY and HY family. As a NATO reporting name, it applies only to the land-based variant of the HY-1.[4]
Development
[edit]

Chinese preparations were underway before receiving the first P-15s and related technical data from the Soviets in 1959. On 8 October 1956, the Fifth Academy was founded - with Qian Xuesen as director - to pursue missile development. In March 1958 a cruise missile test site was selected at Liaoxi in Liaoning.[2]
In November 1960, the first successful missile test was conducted after the withdrawal of Soviet advisors in September, due to the Sino-Soviet split. The P-15 was copied to become the SY-1. In October 1963, production started at the Nanchang Aircraft Manufacturing Company. In 1965, the first successful test occurred. In August 1967, production was approved. The SY-1 entered service by the end of the decade.[2]
The SY-1 was developed into the improved HY-1. In December 1968, the HY-1 was successfully tested, and entered service in 1974.[5]
Operational history
[edit]Iran–Iraq War
[edit]The Silkworm gained fame in the 1980s when it was used by both sides in the Iran–Iraq War. Both countries were supplied by China. In 1987, Iran launched a number of Silkworm missiles from the Faw Peninsula, striking the American-owned, Liberian-flagged tanker Sungari and the U.S.-flagged tanker Sea Isle City in October 1987.[6] Five other missiles struck areas in Kuwait earlier in the year.[7]
In October 1987, Kuwait's Sea Island offshore oil terminal was hit by an Iranian Silkworm, which was observed to have originated from the Faw peninsula. The attack prompted Kuwait to deploy a Hawk missile battery on Failaka Island to protect the terminal.[8] In December 1987, another Iranian Silkworm was fired at the terminal, but it struck a decoy barge instead.[9]
Prior to these attacks the missile's range was thought to be less than 80 kilometres (50 mi), but these attacks proved that the range exceeded 100 kilometres (62 mi) with Kuwaiti military observers seeing that the missiles originated from the area and tracking them on radar along with US satellite imagery of the launch sites.[10]
Persian Gulf War
[edit]On February 25, 1991 during Operation Desert Storm, a shore-based Iraqi launcher fired two Silkworm missiles at the USS Missouri which was in company with the USS Jarrett and HMS Gloucester. A Sea Dart missile from HMS Gloucester shot down one Silkworm and the other missed, crashing into the ocean.[11] Royal Air Force officers subsequently recovered an HY-2 missile at Umm Qasr in southern Iraq. It is currently displayed at the Royal Air Force Museum Midlands.[12]
Iraq War
[edit]During the 2003 invasion of Iraq, Iraq used the Silkworm (HY-2 Seersucker) as a surface to surface missile, by firing at least two of them at the coalition positions in Kuwait.[13]
Blockade of Yemen
[edit]On 12 October 2016, during the Blockade of Yemen, two Silkworm missiles were fired from the Houthi-controlled port of Al Hudaydah at the destroyer USS Mason operating in the Bab el-Mandeb strait. Both impacted the sea, possibly due to the countermeasures.[14][15]
Variants
[edit]SY series
[edit]- SY-1
- License produced version of the P-15 Termit.[2] NATO reporting name CSS-N-1 Scrubbrush.[1]
- SY-2[1]
- NATO reporting names CSS-N-5 Sabot. The SY-2 is a significant redesign of the SY-1 missile and is no longer a copy of the P-15. The missile has a longer airframe and is powered by a solid propellant rocket motor, instead of the liquid propellant design from the Styx. The SY-2 otherwise shares launchers and support equipment with the SY-1 (P-15), however, and eventually replaced the old missiles on unmodernized Jianghu class frigates.[16]
- SY-2A
- An improved SY-2 with a longer range.[16]
- FL-2
- The export version of the SY-2.[16]
HY series
[edit]- HY-1
- NATO reporting names CSS-N-2 Safflower (ship-based) and CSSC-2 Silkworm (land-based.)[1]
- HY-2
- NATO reporting names CSS-N-3 Seersucker (ship-based) and CSSC-3 Seersucker (land-based.)[1]
- HY-3
- Unsuccessful supersonic variant.[17]
- HY-4
- Powered by a WP-11 turbojet, a reverse-engineered Teledyne-Ryan J69-T-41A.[18] Used for LACM development.[19] NATO reporting name Sadsack.[20]
- HY-41
- An improved HY-4.[21]
- C-201
- An export version of the HY-2.[17]
- C-301
- An export version of the HY-3.[22]
- C-201W
- An export version of the HY-4.[17]
- XM-41
- An export version of the HY-41.[21]
Further development
[edit]- YJ-6
- Anti-ship missile developed from the HY-2.
- YJ-63
- Air-launched LACM sharing visual characteristics of the HY-2, HY-4, and YJ-6. 200 km range.[18]
- AG-1
- Longer-ranged variant of the HY-2 developed by North Korea.[23]
Operators
[edit]References
[edit]- ^ a b c d e f Gormley, Erickson & Yuan 2014b, p. 113.
- ^ a b c d Gormley, Erickson & Yuan 2014b, p. 9.
- ^ Gormley, Erickson & Yuan 2014b, p. 28.
- ^ Gormley, Erickson & Yuan 2014b, p. 135.
- ^ Gormley, Erickson & Yuan 2014b, pp. 9–10.
- ^ "U.S. Flag Tanker Struck by Missile in Kuwaiti Waters; First Direct Raid". The New York Times. October 17, 1987.
- ^ "The Gulf Punch, Counterpunch". Time.
- ^ "The Gulf Punch, Counterpunch". Time.
- ^ "Iranian Silkworm strikes decoy barge"; Daniel J. Silva. St. Petersburg Times. St. Petersburg, Fla.: December 8, 1987. p. 14.A.
- ^ Counter-memorial and Counter-claim submitted by the United States of America Archived 2014-03-31 at the Wayback Machine. June 23, 1997.
- ^ Rostker, Bernard (December 2000). "TAB H – Friendly-fire Incidents". Depleted Uranium in the Gulf (II). United States Department of Defense. Archived from the original on 2013-06-01. Retrieved 2007-02-25.
- ^ "Hai Ying 2G Seersucker". RAF Museum. Retrieved 17 May 2014.
- ^ "Center for Defense Information". Project On Government Oversight. Archived from the original on December 23, 2003.
- ^ "Official: Yemen rebels fire 2 missiles at Navy ship, U.S. responds with strikes". CBS News. 2016-10-12. Retrieved 2025-01-12.
- ^ LaGrone, Sam (12 October 2016). "Pentagon Pledges to Respond in 'Appropriate Manner' After New Yemen Missile Attack on USS Mason". USNI News. U.S. Naval Institute. Retrieved 12 October 2016.
- ^ a b c Kopp, Carlo; Andrew, Martin (12 August 2009). "HAIC SY-2/SY-2A/FL-2 / CSS-N-5 Sabot". ausairpower.net: 1.
- ^ a b c Gormley, Erickson & Yuan 2014a, p. 102.
- ^ a b Gormley, Erickson & Yuan 2014b, p. 29.
- ^ Gormley, Erickson & Yuan 2014b, p. 27.
- ^ Gormley, Erickson & Yuan 2014b, p. 84.
- ^ a b Kopp, Carlo; Andrew, Martin (12 August 2009). "CHETA C-201W / HY-4/HY-4A/G / HY-41 / CSS-C-7 Sadsack". ausairpower.net: 1.
- ^ Gormley, Erickson & Yuan 2014a, p. 105.
- ^ "KN-01 (Silkworm/Styx)". Missile Threat. Center for Strategic and International Studies. 31 July 2021. Retrieved 7 July 2022.
Sources
[edit]- Gormley, Dennis M.; Erickson, Andrew S.; Yuan, Jingdong (30 September 2014a). "A Potent Vector: Assessing Chinese Cruise Missile Developments". Joint Forces Quarterly (75). National Defense University.
- Gormley, Dennis M.; Erickson, Andrew S.; Yuan, Jingdong (2014b). A Low-Visibility Force Multiplier: Assessing China's Cruise Missile Ambitions (PDF) (Report). Washington, D.C.: National Defense University Press.
External links
[edit]Silkworm (missile)
View on GrokipediaDevelopment
Origins from Soviet technology
The development of the Silkworm missile series began with Chinese acquisition of Soviet P-15 Termit (NATO: SS-N-2 Styx) anti-ship cruise missile technology in the late 1950s, amid broader Sino-Soviet military cooperation before the 1960 split. This transfer provided China with design blueprints and likely missile samples, forming the basis for indigenous production rather than full-scale exports of complete systems. Chinese engineers at Factory 320 (Nanchang Aircraft Factory) initiated disassembly and adaptation efforts, focusing on replicating the P-15's core liquid-fuel propulsion and radar-guided airframe for coastal defense applications.[9] The initial Chinese variant, designated SY-1 (CSS-N-1 Scrubbrush), emerged as a near-direct copy of the P-15, with preliminary factory testing completed in 1964 and the first flight test conducted in 1965. These milestones marked China's entry into anti-ship cruise missile production, though the SY-1 retained many original Soviet components due to limited domestic manufacturing capabilities at the time. Efforts emphasized shore-based launchers to counter naval threats in the Taiwan Strait, establishing a foundational platform for subsequent iterations without significant modifications to the baseline design.[9][10] Progress stalled during the Cultural Revolution (1966–1976), a period of political upheaval that purged technical experts, disrupted industrial coordination, and prioritized ideological campaigns over military R&D, thereby postponing SY-1 operational deployment until the mid-1970s. This internal chaos compounded challenges from the earlier Great Leap Forward, limiting sustained testing and serial production despite initial prototypes. Restoration of specialized teams post-1976 enabled resumption, but the decade-long interruption underscored vulnerabilities in China's nascent missile sector reliant on foreign-derived technology.[11][12]Chinese production and early testing
Following the Sino-Soviet split, China initiated reverse engineering of the Soviet P-15 Termit (SS-N-2 Styx) anti-ship missile in the early 1960s, utilizing available samples to develop indigenous production capabilities.[1] The initial variant, designated SY-1 (CSS-N-1 Scrubbrush), underwent factory tests in August 1964, demonstrating basic flight and guidance functionality derived from the Soviet design.[13] However, early iterations faced reliability challenges inherent to the rapid adaptation of foreign technology, including inconsistencies in propulsion stability and seeker performance under varied sea conditions.[1] By the late 1960s, the SY-1 had entered limited service as China's first domestically produced anti-ship cruise missile, primarily for coastal defense applications.[14] To address shortcomings in range and structural integrity, development shifted toward the improved HY-1 (CSS-N-2 Safflower) variant around 1970, incorporating enhancements to the airframe and liquid-fuel rocket motor for better stability and extended operational reach.[1] Final design testing for the HY-1 achieved six hits out of seven firings in 1970, indicating hit probabilities exceeding 70% under controlled conditions, though real-world factors like target maneuvering would reduce effectiveness.[15] The HY-1 was certified for production and entered service in 1974, marking the maturation of China's early anti-ship missile program.[16] Integration efforts under Project 021 focused on adapting the missiles for Type 021-class fast attack craft, which were indigenous copies of Soviet Osa-class boats, enabling tube-launched SY-1 deployments.[1] Parallel work incorporated elevating launchers for HY-1 coastal batteries, overcoming logistical hurdles in transporter-erector alignment and battery mobility to support layered shoreline defense.[1] These advancements laid the groundwork for operational deployment, despite persistent limitations in accuracy compared to later systems.[13]Major upgrades and export adaptations
The HY-2 variant, introduced in 1975, featured a stretched airframe compared to the earlier HY-1, extending the missile's range to approximately 95 kilometers while maintaining liquid-fueled propulsion and radar guidance.[17] This upgrade addressed limitations in the Soviet-derived P-15 design by increasing fuel capacity through a longer fuselage, enabling greater standoff distances for coastal defense roles.[1] Export adaptations under the C-201 designation simplified certain electronics and seeker components to enhance reliability in environments with limited technical support, prioritizing robustness over cutting-edge precision for recipient nations deploying in asymmetric conflicts.[8] These modifications included hardened radar systems less susceptible to environmental interference, facilitating integration onto basic launch platforms without requiring advanced calibration infrastructure.[15] In the 1990s, the HY-2G upgrade incorporated a high-precision radio altimeter, reducing sea-skimming altitude to 30–50 meters during level flight to evade radar detection and improve terminal-phase survivability against defenses.[15] This enhancement, distinct from domestic inertial refinements, focused on export viability by boosting penetration against modern naval countermeasures while retaining compatibility with legacy systems.[18]Design and technical specifications
Airframe, propulsion, and flight profile
The Silkworm missile employs a robust, cylindrical airframe optimized for subsonic anti-ship operations, featuring a streamlined fuselage that integrates fuel tanks, engine components, and structural reinforcements for withstanding launch stresses and sea-skimming dynamics. Standard dimensions across early variants include a body length of approximately 5.8 meters, a diameter of 0.76 meters, and a wingspan of 2.4 meters with folding cruciform wings and tail surfaces for aerodynamic stability and control during cruise. Launch weights typically range from 2,100 to 2,300 kilograms, reflecting the inclusion of propellants and onboard systems that prioritize simplicity and reliability over advanced materials.[19][20] Propulsion consists of a tandem configuration: an underbody solid-propellant booster rocket provides initial thrust for launch and acceleration to flight speed, separating shortly after ignition, while the main stage utilizes a liquid rocket engine fueled by storable hypergolic propellants, such as unsymmetrical dimethylhydrazine (UDMH) and inhibited red fuming nitric acid (IRFNA). This setup delivers sustained thrust for the majority of the trajectory, achieving speeds up to Mach 0.9, but imposes inherent limitations on agility due to binary burn phases without variable thrust or extended loiter capability. The hypergolic nature ensures reliable ignition without external oxidizers, though it contributes to corrosion risks over time from residual propellants.[21][1] The operational flight profile commences with booster-driven ascent, transitioning to sustainer propulsion for a mid-profile climb to cruising altitudes of 100 to 300 meters, which balances fuel efficiency and radar horizon extension. Terminal descent shifts to a sea-skimming envelope at 10 to 50 meters above the wave tops, exploiting low observables for terminal approach while the fixed-thrust rocket engine dictates a predictable, ballistic-influenced path with minimal evasive potential. This profile, constrained by the airframe's inertial stability and propulsion envelope, supports ranges up to 40 to 80 kilometers in baseline configurations, emphasizing volume fire over precision maneuvering.[19][22]