The Hy-1 and HY-2 anti ship missiles.
these are older than the ones posted earlier, nevertheless they are big and powerful
if they make it through the defenses, but more importantly these a effective against oil tankers.
HY-1 ( CSS-N-1/CSS-C-2 Silkworm)This is a development of the SY-1 which itself is a Chinese reversed engineered Russian Styx (P-15) missile. Iran may have received these obsolete missiles in the early1980's but i cant find any hard numbers.* It was the HY-2 that seems to be the more important missile in term of real numbers.
The HY-1 is
the silkworm missile, while related missiles including the SY-1 and HY-2 also get
called this in western sources (and even completely different ones like the
C-802 in my last post)
, they actually have their own designations. I must also note; there seems to be a bit nore confusion between the HY-1 and 2 in particular. In some cases they get grouped up purposely and treated as one.
* Iran has been
reported to have them in stock in some sources.
"While the SY-1 is a rather direct copy of the P-15 missile, the HY-1 features some improvements including a lengthened fuel tank for extended range and modified autopilot for better accuracy. The missile is 760mm longer than the SY-1 and its range has increased from 40km to 70km.
VARIANTS
Variants |
Description |
HY-1 |
Basic variant land-to-ship missile developed from the Soviet P-15 (SS-N-2 Styx) |
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 |
Target drone for the test of HQ-2A SAM |
HJ-1YB |
Target drone for the test of HQ-61 SAM |
MISSILE
The HY-1 is almost identical to the SY-1/SS-N-2 in appearance apart from the slightly longer missile body. The missile features a round nose accommodating the radar seeker, a pair of mid-mounted delta wings on the middle section of 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 missile requires fairly complex maintenance due to its use of liquid rocket. The missiles large warhead can sink or severely damage a 3,000t-class destroyer.
SPECIFICATIONS
Dimensions: Length: 6.60m; Diameter: 0.76m; Wingspan: 2.4m
Launch weight: 2,300kg
Warhead: 513kg shape charged high-explosive
Propulsion: One liquid rocket engine and one solid rocket booster
Max speed: Mach 0.8
Max range: 70km
Flight altitude: 100~300m (early models); <20m (later models)
Guidance: Inertial + active conical scanning terminal guidance radar (early models); or inertial + monopulse active radar (later models)
Single-hit probability: 70%"
Diagram from
www.kimsoft.com
HY-2 (CSS-C-3 Seersucker) or C-201
"The missile was based on the HY-1 anti-ship missile with extended range and improved accuracy. Only land-based variant has been developed due to its large size. As well as serving with the PLA Navy Coastal Defence Force, the missile was exported to the Middle East in significant numbers in the 1980s."
Variants |
Description |
HY-2 |
Also known as C-201 in its export name. 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 (a more sensitive IR seeker and a higher precision radio altimeter and new auto-pilot to lower the level flight altitude) |
HY-2B |
Improved radar-guidance variant with a mono-pulse radar seeker replacing the original conical scanning radar |
HY-2BII |
Improved variant of the HY-2B with a newly designed radar seeker |
C-201W |
Extended-range variant powered by a turbojet engine replacing the original liquid-fuel rocket motor. Export only |
Iranian launched Seersucker
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 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 land-based launcher and flies at an altitude of 1,000m during the initial stage of the flight. After the missile switched to the cruising mode, the flight altitude was reduced to 100~300m. During the final stage of the flight, the missile switched on its radar seeker and dives to an altitude of 8m until it hits the target.
Dimensions: Length: 7.48m; Diameter: 0.76m; Wingspan: 2.4m
Launch weight: 2,998kg
Warhead: 513kg shape charged high-explosive
Propulsion: One liquid rocket engine and one solid rocket booster
Max speed: Mach 0.8
Max range: 95~100km
Flight altitude: 100~300m (early models); <20m (later models)
Guidance: Inertial + active conical scanning terminal guidance radar (HY-2); or inertial + IR guidance (HY-2A); or inertial + monopulse active radar (HY-2B)
Single-shot hit probability: 90%
SinodefenceRange of these missiles (HY-2) in the Persian gulf.
found this on a right wing
blog.
what has numbers in Iran?In early 1988 Iran claimed the capacity to manufacture HY-2s and other antiship cruise missiles indigenously. It is currently estimated that Iran has about 100 HY-2 missiles on eight to ten mobile missile launchers deployed on the north side of the Straits of Hormuz.
SourceNumber deployed about 310 HY-2 ship-launcher, 50 coastal defense installations.
sourceDeliveries look like the 300+ number might be more right as well as deployments on other island wiith the gulf. (
Source)
..and bit more on the Iran's HY-X alleged capability.
"
Bandar Abbas hosts a missile site overseen by the Islamic Revolutionary Guard Corps (IRGC) Navy Command. The Chinese built this facility in 1987. The facility assembles and extends the range of Silkworm missiles, modifies Seersucker missiles, and manufactures rockets. The Chinese may be assisting the IRGC in extending the range to 400km. Bandar Abbas also is believed to host a launch site with three to six launchers for the land-based Silkworm." Link
Edited by Hellios - 04-Mar-2007 at 00:06