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Military


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
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%


NameAspide 2000 (aka: Aspide Mk II)
Date of Introduction1986 for Mk I
ProliferationAt Least 18 Countries
TargetFW, heli, CM, UAV, ASM, bombs
RangeMax. Range: 45
RangeMin. Range: 0.75 km
AltitudeMax. Altitude: 6,000+
RangeMin. Altitude: 10
DimensionsLength (m): 3.65
Diameter (mm) 203
Weight230 kg
Missile Speed1,288 m/s
Velocity4.0 mach
Maneuver Capability35-40 Gs
PropulsionSolid fuel booster
GuidanceJ-band semi-active radar homing, active or passive homing, and home-on-jam
Warhead TypeFrag-HE
Warhead Weight33 kg
Fuze TypeProximity and Contact
Probability of Hit80 FW and heli Ph%
Simultaneous missiles2 per Target
Reaction Time11 sec
Time Between LaunchesINA sec
Fire on MoveNo
Number of Fire Channels2



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Page last modified: 28-04-2019 18:50:12 ZULU