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HY-3 (CSS-C-6 Sawhorse) Chinese Short-Range Anti-Ship Cruise Missile

HY-3

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Basic Information
Name
HY-3 (CSS-C-6 Sawhorse) Chinese Short-Range Anti-Ship Cruise Missile
Designation
HY-3
Alternate Designation
Equipment Type
Manufacturer
Date of Introduction
1985
Description

The HaiYing-3 (HY-3, also known as C-301 in its export name; NATO codename: CSS-C-6 Sawhorse) is the active radar homing, ramjet-powered supersonic land-to-ship missile developed by China Haiying Electro-Mechanical Technology Academy (CHETA, also known as 3rd Space Academy). The missile was developed in the 1980s based on the design of the HY-2 (C-201) and the ramjet technology of the cancelled YJ-1 (C-101). The development was completed in the early 1990s but the missile did not enter service. The HY-3 is a large-size missile with a slim forward body and sharp nose, and a fatter rear half with four solid rocket boosters and two ramjet engines located aft of the missile body. There are a pair of front-canards on the front fuselage, four control surfaces on the rear fuselage, and four smaller stabilizing fins attached on the solid rocket boosters. The booster motors accelerate the missile to past Mach 1.8 and the kerosene-fueled ramjet engines accelerate the missile to a cruise speed of Mach 2.0. Its range is variously reported as up to 130 km, and it can fly as low as 50 m in its terminal attack phase. The missile is programmed to dive from cruising altitude to under 30m before the active-radar terminal phase begins, then dive onto the target just prior to impact. The 3.5 ton missile is launched from a land-based launcher. Each firing unit consists of four launchers, a target acquisition radar, a fire-control unit, a power unit, and 8~12 missile reloading vehicle (each with one missile).

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-3 (CSS-C-6 Sawhorse) Anti-Ship Cruise Missile
Missile
Name HY-3; NATO: CSS-C-6 Sawhorse
Type Anti-Ship Cruise Missile
Basic Load INA
Manufactuer Nanchang Aircraft Factory (Chinese)
Length 9.85m
Diameter 0.76 m
Wingspan 2.24 m
Weight, Total 3,400 kg
Warhead Type Shaped charge high explosive
Warhead Weight 500 kg
Propulsion Two side-mounted ramjet engines; four solid propellant boost motors
Speed Mach 2.5
Range 180 km
Cruising Altitude 50 meters
Guidanc System Inertial and terminal active radar
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
Operators (5)
China
Iran
Bangladesh
Cuba
Sudan
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