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HY-4 (SSC-7 Sadsack) Chinese Short-Range Anti-Ship Cruise Missile Chinese Short-Range Anti-Ship Cruise Missile

HY-4

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Basic Information
Name
HY-4 (SSC-7 Sadsack) Chinese Short-Range Anti-Ship Cruise Missile Chinese Short-Range Anti-Ship Cruise Missile
Designation
HY-4
Alternate Designation
Equipment Type
Manufacturer
Nanchang Aircraft Factory
Date of Introduction
1983
Description

The HY-4 (SSC-7 Sadsack) Chinese Short-Range Anti-Ship Cruise Missile development of the C-201 is a mid-range ground-, air-, and ship-launched cruise missile. Development of the HY-4 is believed to have started in the mid-1970s, replacing the C-201 HY-2 liquid propellant sustainer motor with a small turbojet engine, and adding a monopulse active radar seeker. Apart from the substitution of the turbojet engine, the overall configuration of the HY-4 variant of the C-201 missile is similar to the HY-2 variants of the C-201, with two delta wings and tri-form rudder and tail. The missile has a radar altimeter which allows the cruise height to be varied between 70 and 200 m altitude, followed by a steep dive onto the target. The air-launched version is designated as C-401.

Air & Air Defense Specifications
Max Speed 1048.1 km/h
Range 500.0 km
Variants
HY-1 Basic developmental version developed from the SY missiles, used only in very small numbers as land-to-ship missile for evaluation purposes. Did not enter series production and was replaced by HY-1J.
HY-1J Ship-to-ship variant for Type 051 DDG
HY-1JA Improved ship-to-ship variant with a new radar seeker for better anti-jamming capability and accuracy
HY-1A Land-to-ship variant based on the HY-1JA
HY-1B Low level target drone for the test of HQ-2A SAM
HJ-1YB Target drone for the test of HQ-61 SAM
HY-4 (CSS-C-7) Sadsack Anti-Ship Cruise Missile
Missile
Name HY-4; NATO: SSC-7 Sadsack
Type Anti-Ship Cruise Missile
Basic Load INA
Manufactuer Nanchang Aircraft Factory (Chinese)
Length 7.36 m
Diameter 0.76 m
Wingspan 2.4 m
Weight, Total 1,740 kg
Warhead Type Shaped charge high explosive
Warhead Weight 513 kg
Propulsion one turbojet engine and one solid rocket booster
Speed Mach 0.8 – 0.85
Range 500 km
Cruising Altitude The missile has a radar altimeter which allows the cruise height to be varied between 70 and 200 m altitude, followed by a steep dive onto the target.
Guidanc System Inertial + active conical scanning terminal guidance radar (early models); or inertial + monopulse active radar (later models)
Single-Shot Kill Probability 70%
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
7.36 m
Width
2.4 m
Height
Weight
1740 kg
Operators (1)
Bangladesh
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