Hi comrades, I found that HY-3, HF-3 of China and Taiwan seemed rooted Moskit P-270 missiles from Russia. Aerodynamic design, shape, ramjet engines are all the same.
The only difference is support for multi Moskit braided discharge system, aircraft (up to range of 250 km range), surface warships and land.
Specifications
Weight 3.4 ton
Length 9.85 meter
Warhead 500 kg warhead
Detonation
mechanism Semi-armor piercing
Engine rocket motor
Propellant liquid fuel
Operational
range 130 - 180 km
Flight altitude 50 cruising
Speed Mach 2.5
Guidance
system ARH & IR
Launch
platform Ground
Specifications
Type: Anti-ship missile
Range: 130 Kilometers
Flight altitude: 125-250 Meters (test up to Mach 3 and range of 400km)
Power Plant: Rocket-Ramjet
Top Speed: 2300 km/h
Length: Approx. 6.096 m[1]
Diameter: .4572 m[1] Missile Body Only
Weight: 3,000-3,300 lbs[1]
Guidance: Inertial with terminal active (X-Band) radar homing[1]
Date Deployed: 12/2007 250 Units - approved for official low rate production as of 1/2008
Specifications
Weight kg 4,500 kg (9,900 lb)
Length 9.745 m (31.97 ft)
Diameter 0.8 m (2.6 ft)
Warhead 320 kg (710 lb) explosive or 120 kt of TNT fission-fusion thermonuclear
Engine Four ramjets (solid fuel rocket on air-to-surface version)
Wingspan 2.10 m (6.9 ft)
Operational
range 120 km - 250 km
Flight altitude 20 m (66 ft) above sea level
Speed Mach 3[1]
Guidance
system active radar
Launch
platform naval ships, fixed-wing aircraft
The only difference is support for multi Moskit braided discharge system, aircraft (up to range of 250 km range), surface warships and land.
Specifications
Weight 3.4 ton
Length 9.85 meter
Warhead 500 kg warhead
Detonation
mechanism Semi-armor piercing
Engine rocket motor
Propellant liquid fuel
Operational
range 130 - 180 km
Flight altitude 50 cruising
Speed Mach 2.5
Guidance
system ARH & IR
Launch
platform Ground
Specifications
Type: Anti-ship missile
Range: 130 Kilometers
Flight altitude: 125-250 Meters (test up to Mach 3 and range of 400km)
Power Plant: Rocket-Ramjet
Top Speed: 2300 km/h
Length: Approx. 6.096 m[1]
Diameter: .4572 m[1] Missile Body Only
Weight: 3,000-3,300 lbs[1]
Guidance: Inertial with terminal active (X-Band) radar homing[1]
Date Deployed: 12/2007 250 Units - approved for official low rate production as of 1/2008
Specifications
Weight kg 4,500 kg (9,900 lb)
Length 9.745 m (31.97 ft)
Diameter 0.8 m (2.6 ft)
Warhead 320 kg (710 lb) explosive or 120 kt of TNT fission-fusion thermonuclear
Engine Four ramjets (solid fuel rocket on air-to-surface version)
Wingspan 2.10 m (6.9 ft)
Operational
range 120 km - 250 km
Flight altitude 20 m (66 ft) above sea level
Speed Mach 3[1]
Guidance
system active radar
Launch
platform naval ships, fixed-wing aircraft
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