رد: معركة اللاذقية البحرية 1973 بين سورية واسرائيل
ليس صيني اخي العزيز انما اوكراني و يطلق عليه في القوات البحرية بي 21 الراداري نشط مطور و حراري و يطلق عليه بي 22 و يوجد النسخة الروسية القديمة مع تطويرات علي برنامج الطيران الآلي و الرادار و تطوريات علي محرك الصاروخ و يطلق عليه بي 15
مرحبا صديقي العزيز هو p20 اخذته الصين وصممت عليه السيلك وورم
P-20M: A surface version of the P-20L with folding wings. This was the definitive version of the P-15M with radar guidance.
The Chinese used this missile as a basis for their Silkworm series, with IR, radar and turbojets or rocket engines depending on the model.
According to a press report from June 1990, China has signed a protocol with Egypt to help modernize the Sakr missile factory, "enabling it to produce a newer version of Soviet antiaircraft missiles, the surface-to-surface Scud-B and Silkworm and the Egyptian Sakr rockets."
Some reports suggest the FL-1 entered service with the Chinese Navy in 1980 and that it has been exported to Bangladesh, Pakistan, Thailand and Egypt (SY-1/HY-1).
وولتنويه هنا فالسيلك وورم هو النوع المخصص لدفاع الساحلي CSS-N-2 Safflower
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SY-1]
This is the original Chinese version of Soviet P-15 Termit missile, and the first was SY-1, produced at Factory 320 (the Nanchang Aircraft Factory [南昌飞机制造厂]);; Chinese sources identify the designers as Li Tongli and Lu Lin. The main difference between P-15 Termit and SY-1 missiles is that the unreliable aneroid altimeter of P-15 Termit was replaced by a much more reliable radar altimeter in SY-1. The successor of SY-1, designed by Peng Lisheng (彭历生) and designated as SY-1A, had a mono-pulse terminal guidance radar seeker replacing the original conical scanning radar seeker. The missile received a NATO reporting name CSS-N-1 Scrubbrush.
The missile has been upgraded to be air-launched, and the air-launched version is known as C-601, which is the first air-launched anti-ship missile in China. The missile received a NATO reporting name CAS-1 Kraken. It was used by Iraqi H-6 during Iran-Iraq War. An upgraded version that is fully solid state with integrated circuitry and new active radar seeker and new radar altimeter entered service as SY-1A in early 1980s.
Specifications:
Length: 6.55 metre
Diameter: 0.76 metre
Wingspan: 2.4 metre
Weight: 2,095 kg
Warhead: 513 kg shaped charge high explosive
Propulsion: One liquid rocket engine and one solid rocket booster
Speed: Mach 0.8
Range: 150 km [1]
Cruising altitude: < 20 meters
Guidance: Inertial + active conical scanning terminal guidance radar (SY-1); or inertial + monopulse active radar (SY-1A)
Single-shot kill probability: 70%
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HY-1]
The HY-1 received two separate NATO reporting name, the CSS-N-2 Safflower for the ship to ship version and the CSSC-2 Silkworm for the land based coastal defense variant.
The HY-1J was intended for use on the Type 051 destroyers. However, the turmoil of the Cultural Revolution prolonged development into the 1980s. As a result, the Type 051s deployed into the Pacific Ocean to support ballistic missile tests without anti-ship missiles.
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
Specifications
Length: 6.60 metre
Diameter: 0.76 metre
Wingspan: 2.4 metre
Weight: 2,300 kg
Warhead: 513 kg shaped charge high explosive
Propulsion: One liquid rocket engine and one solid rocket booster
Speed: Mach 0.8
Range: 85 km
Cruising 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-shot kill probability: 70%
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