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HY-2 (SSC-3) Seersucker Chinese Short-Range Anti-Ship Cruise Missile

HY-2

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Basic Information
Name
HY-2 (SSC-3) Seersucker Chinese Short-Range Anti-Ship Cruise Missile
Designation
HY-2
Alternate Designation
Equipment Type
Manufacturer
Nanchang Aircraft Factory
Date of Introduction
1975
Description

The HY-2 (SSC-3) Seersucker Chinese Short-Range Anti-Ship Cruise Missile is identical to the HY-1 but with a further stretched body. The missile features a round nose accommodating the radar seeker, a pair of mid-mounted delta wings on the middle section of the missile body, and three tail control surfaces. The missile is powered by a liquid-fuel rocket motor, with a solid rocket booster attached under the missile fuselage. The HY-2 is launched from the land-based launcher and flies at an altitude of 1000 m during the initial stage of the flight. After the missile switched to the cruising mode, the flight altitude was reduced to 100 ~ 300 m. During the final stage of the flight, the missile switched on its radar seeker and dives to an altitude of 8 m until it hits the target. The single-shot hit probability is estimated to be 90%. Due to its oversized body, the HY-2 did not develop a ship-to-ship variant. The missile is obsolete and will be replaced by the YJ-8 series in the future.

Air & Air Defense Specifications
Max Speed 987.8 km/h
Range 200.0 km
Variants
HY-2 Basic variant radar-guidance land-to-ship missile *developed from the HY-1 missile.
HY-2A IR-guidance variant.
HY-2AII Improved variant of the HY-2A.
HY-2B Improved radar guidance variant with a monopulse radar seeker replacing the original conical scanning radar.
HY-2BII Improved variant of the HY-2B with a newly designed radar seeker.
C-201 Export designation for HY-2.
C-201W Extended-range variant powered by a turbojet engine replacing the original liquid-fuel rocket motor. Export only.
YJ-6 Air launched variant of the HY-2.
YJ-61 Improved variant of the YJ-6.
HY-2 (CSS-C-3 Seersucker) Anti-Ship Cruise Missile
Missile
Name HY-2; NATO: SSC-3
Type Anti-Ship Cruise Missile
Basic Load INA
Manufactuer Nanchang Aircraft Factory (Chinese)
Length 7.48 m
Diameter 0.76 m
Wingspan 2.4 m
Weight, Total 2,998 kg
Warhead Type Shaped charge high explosive
Warhead Weight 513 kg
Propulsion One liquid rocket engine and one solid rocket booster
Speed Mach 0.8
Range 200 km
Cruising Altitude < 20 meters
Guidanc System Inertial + active conical scanning terminal guidance radar (HY-2); or inertial + infrared homing guidance (HY-2A); or inertial + monopulse active radar (HY-2B)
Single-Shot Kill Probability 90%
Details
Country of Origin China
Category Short-Range Cruise Missiles (SRCM) (Less than 600 km)
Air > Short-Range Cruise Missiles (SRCM) (Less than 600 km)
Filter Label
H
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
7.48 m
Width
0.76 m
Height
Weight
2998 kg
Operators (6)
China
Iran
Bangladesh
Cuba
Myanmar
Sudan
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