WEG MediaWiki

HY-4 (CSS-C-7) Sadsack Chinese Anti-Ship Cruise Missile

tiers
false
false
true
false
categories
"WEG"
"Cruise Missiles"
"Short-Range Cruise Missiles (SRCM) (Less than 600 km)"
"Vessel-Launched Cruise Missiles (VLCM) (Less than 600 km)"
"China, People's Republic of"
"PRO_Bangladesh"
"Air"
"Tier3"
notes"The HY-4 development of the C-201 is a mid-range ground-, air-, and ship-launched cruise missile. Development of the C-201 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"
dateOfIntroduction1983
countryOfOrigin"China, People's Republic of"
proliferation"Bangladesh"
selectedregions
"All Regions"
checkedregions
Empty array
checkedcountries
"Bangladesh"
dis
name"Unknown"
string"00.00.000.000.000.000.000"
images
"HY-4_(CSS-C-7)_Sadsack(A).jpg"
"HY-4_(CSS-C-7)_Sadsack(B).jpg"
sections
name"System"
properties
name""
value""
name""
value""
name""
value""
name"HY-4 (CSS-C-7) Sadsack Anti-Ship Cruise Missile"
sections
name"Missile"
properties
name"Name"
value"HY-4; NATO: CSS-C-7 Sadsack"
name"Type"
value"Anti-Ship Cruise Missile"
name"Basic Load"
value"INA"
name"Manufactuer"
value"Nanchang Aircraft Factory (Chinese)"
name"Length"
value"7.36 m"
name"Diameter"
value"0.76 m"
name"Wingspan"
value"2.4 m"
name"Weight, Total"
value"1,740 kg"
name"Warhead Type"
value"Shaped charge high explosive"
name"Warhead Weight"
value"513 kg"
name"Propulsion"
value"one turbojet engine and one solid rocket booster"
name"Speed"
value"Mach 0.8 – 0.85"
name"Range"
value"500 km"
name"Cruising Altitude"
value"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."
name"Guidanc System"
value"Inertial + active conical scanning terminal guidance radar (early models); or inertial + monopulse active radar (later models)"
name"Single-Shot Kill Probability"
value"70%"
variants
name"HY-1"
notes"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."
name"HY-1J"
notes"Ship-to-ship variant for Type 051 DDG"
name"HY-1JA"
notes"Improved ship-to-ship variant with a new radar seeker for better anti-jamming capability and accuracy"
name"HY-1A"
notes"Land-to-ship variant based on the HY-1JA"
name"HY-1B"
notes"Low level target drone for the test of HQ-2A SAM"
name"HJ-1YB"
notes"Target drone for the test of HQ-61 SAM"
type"WEG"
version1
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