¾Õ¼ ¸îÂ÷·Ê ¿Ã¸° FNSS Pars II (Leopard) Àå·û½ÄÀå°©Â÷ÀÔ´Ï´Ù.
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Technical:
Engine...................................... 500 hp - 600 hp Diesel
Transmission.............................. Fully Automatic
Number of Forward and
Reverse Speed............................ 7 Forward 1 Reverse
Power to Weight Ratio................... 20.4 to 24.5 hp/ton
EURO Norm of Power Pack............... EURO 3
Power Pack Compliant with
NATO Single Fuel Concept.............. Aviation F34 Fuel
Number of Axles.......................... 4
Driven Axles............................... All
Steered Axles............................. 1,2,3,4
Transfer Case (Shift on Fly)............ 2 Speed
Suspension................................ Semi-Automatic Pneumatic Computer Controlled &
.............................................Adjustable Disc, Hydraulic
Brakes
- Service.................................. In Board Disc, Air/Hydraulic with ABS at Each Wheel
- Parking.................................. Integral to Driveline, Spring Activated,
............................................. Hydraulically Released
Electrical System (Available Power)
- 3 KW 220V AC
- 420 Amp 24V DC
- 30 Amp 12V DC
Tire Type................................. Heavy Duty 1600 R20
Performance:
Max. Road Speed........................ 100 km/h
Creep Speed............................. 3 km/h
Swimming................................. 10 km/h
Fording................................... 1.50 m
Range..................................... 1000 km
Angle of Approach...................... 50¢ª
Angle of Departure..................... 45¢ª
Gradient.................................. 70%
Side Slope................................. 60%
Vertical Obstacle......................... 0.70 m
Trench.................................... 2.40 m
General:
Crew ...................................... 14
Combat Weight......................... 24,494 kg
Empty Weight........................... 16,130 kg
Length.................................... 7.96 m
Width..................................... 2.7 m
Height.................................... 2.17 m
Ground Clearance...................... 0.400 m
Payload................................... 8,364 kg
Air Transportation..................... C130, A400, C17 & C5
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Èò²¿¸®¼ö¸® | 2005-10-03 | Ãßõ 0