صحنه ای از اصابت این موشک به هدف تمرینی
مشخصات این موشک:
Primary Function: |
Long-range subsonic cruise missile for attacking land targets. |
Contractor: |
Hughes Missile Systems Co., Tucson, Ariz. |
Power Plant: |
Williams International F107-WR-402 cruise turbo-fan engine; solid-fuel booster |
Length: |
18 feet 3 inches (5.56 meters); with booster: 20 feet 6 inches (6.25 meters) |
Weight: |
2,650 pounds (1192.5 kg); 3,200 pounds (1440 kg) with booster |
Diameter: |
20.4 inches (51.81 cm) |
Wing Span: |
8 feet 9 inches (2.67 meters) |
Range: |
Land attack, conventional warhead: 600 nautical miles (690 statute miles, 1104 km) |
Speed: |
Subsonic - about 550 mph (880 km/h) |
Guidance System: |
Inertial and TERCOM |
Warheads: |
Conventional: 1,000 pounds Bullpup, or
Conventional submunitions dispenser with combined effect bomblets, or
WDU-36 warhead w/ PBXN-107 explosive & FMU-148 fuze, or
200 kt. W-80 nuclear device |
Date Deployed: |
1983 |
Costs |
$500,000 - current production Unit Cost
$1,400,000 - average unit cost (TY$)
$11,210,000,000 - total program cost (TY$) |
Total Program |
4 170 missiles |
Location: | Tehran-Mehrabad |
Temperature: | 12 °C |
Comfort Level: | 9 °C |
Dew point: | -6 °C |
Pressure: | 1016 millibars |
Humidity: | 28% |
Wind: | 30 km/h from 300° West-northwest |
Last update: | Sat 12:30 IRST |
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