Aspide Mk1/Mk2
Specifications | ||
---|---|---|
Manafacturer | Selenia | |
Date Deployed | 1987 | |
Range | 75 km | |
Ceiling | 8000 m above the launch point | |
Speed | Mach 4 / 4680 km/h | |
Propulsion | One SNIA-Viscosa solid-propellant rocket motor | |
Guidance | Selenia monopulse semi-active radar homing | |
Warhead | 72.75 lb ( 33 kg ) SNIA Difesa e Spazio blast/fragmentation : doppler proximity- and direct action-fuzed |
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Launch Weight | 485 lb ( 220 kg ) 230 kg | |
Length | 12 ft, 1.67 in ( 3.70 m ) 3.65 m | |
Diameter | 8 in ( 203 mm ) 210 mm | |
Fin Span | 3 ft, 3.4 in ( 1.00 m ) same | |
Capacity discovery radar | 20 Km | |
N. fire channels | 2 | |
N. ready missiles to the launch | 12 | |
Time reaction arranges | 11 sec | |
The maximum capacity | 10 Km | |
Minimal capacity | 750 m | |
The maximum quota | 3.5 Km approximately | |
Guidance system | homing semiactive | |
Weight of the missile | 220 Kg approximately | |
maximum speed of the missile | 650 m/sec | |
Single-shot hit probability (SSKP) | 80% |
Name | Aspide 2000 (aka: Aspide Mk II) |
Date of Introduction | 1986 for Mk I |
Proliferation | At Least 18 Countries |
Target | FW, heli, CM, UAV, ASM, bombs |
Range | Max. Range: 45 |
Range | Min. Range: 0.75 km |
Altitude | Max. Altitude: 6,000+ |
Range | Min. Altitude: 10 |
Dimensions | Length (m): 3.65 |
Diameter (mm) | 203 |
Weight | 230 kg |
Missile Speed | 1,288 m/s |
Velocity | 4.0 mach |
Maneuver Capability | 35-40 Gs |
Propulsion | Solid fuel booster |
Guidance | J-band semi-active radar homing, active or passive homing, and home-on-jam |
Warhead Type | Frag-HE |
Warhead Weight | 33 kg |
Fuze Type | Proximity and Contact |
Probability of Hit | 80 FW and heli Ph% |
Simultaneous missiles | 2 per Target |
Reaction Time | 11 sec |
Time Between Launches | INA sec |
Fire on Move | No |
Number of Fire Channels | 2 |
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