WEG MediaWiki

HY-2 (CSS-C-3 Seersucker) Chinese Anti-Ship Cruise Missile

tiers
false
false
true
false
categories
"WEG"
"Cruise Missiles"
"Short-Range Cruise Missiles (SRCM) (Less than 600 km)"
"Ground-Launched Cruise Missiles (GLCM) (Less than 600 km)"
"China, People's Republic of"
"PRO_Bangladesh"
"PRO_China"
"PRO_Cuba"
"PRO_Iran (Islamic Republic of)"
"PRO_Myanmar"
"PRO_Sudan"
"Air"
"Tier3"
notes"The HY-2 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 The missile is obsolete and will be replaced by the YJ-8 series in the future."
dateOfIntroduction1975
countryOfOrigin"China, People's Republic of"
proliferation"Bangladesh, China, Cuba, Iran (Islamic Republic of), Myanmar, Sudan"
selectedregions
"All Regions"
checkedregions
Empty array
checkedcountries
"Bangladesh"
"China"
"Cuba"
"Iran (Islamic Republic of)"
"Myanmar"
"Sudan"
dis
name"CSSC 3A SEERSUCKER LAUNCHER"
string"01.01.045.005.016.002.001"
images
"HY-2_Missile_(B).jpg"
"HY-2_Missile_(A).jpg"
sections
name"System"
properties
name""
value""
name""
value""
name""
value""
name"HY-2 (CSS-C-3 Seersucker) Anti-Ship Cruise Missile"
sections
name"Missile"
properties
name"Name"
value"HY-2; NATO: CSS-C-3 Seersucker"
name"Type"
value"Anti-Ship Cruise Missile"
name"Basic Load"
value"INA"
name"Manufactuer"
value"Nanchang Aircraft Factory (Chinese)"
name"Length"
value"7.48 m"
name"Diameter"
value"0.76 m"
name"Wingspan"
value"2.4 m"
name"Weight, Total"
value"2,998 kg"
name"Warhead Type"
value"Shaped charge high explosive"
name"Warhead Weight"
value"513 kg"
name"Propulsion"
value"One liquid rocket engine and one solid rocket booster"
name"Speed"
value"Mach 0.8"
name"Range"
value"200 km"
name"Cruising Altitude"
value"< 20 meters"
name"Guidanc System"
value"Inertial + active conical scanning terminal guidance radar (HY-2); or inertial + infrared homing guidance (HY-2A); or inertial + monopulse active radar (HY-2B)"
name"Single-Shot Kill Probability"
value"90%"
variants
name"HY-2"
notes"Basic variant radar-guidance land-to-ship missile *developed from the HY-1 missile."
name"HY-2A"
notes"IR-guidance variant."
name"HY-2AII"
notes"Improved variant of the HY-2A."
name"HY-2B"
notes"Improved radar guidance variant with a monopulse radar seeker replacing the original conical scanning radar."
name"HY-2BII"
notes"Improved variant of the HY-2B with a newly designed radar seeker."
name"C-201"
notes"Export designation for HY-2."
name"C-201W"
notes"Extended-range variant powered by a turbojet engine replacing the original liquid-fuel rocket motor. Export only."
name"YJ-6"
notes"Air launched variant of the HY-2."
name"YJ-61"
notes"Improved variant of the YJ-6."
type"WEG"
version1
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