เลือกภาษาไทย | | |
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Thai เลือกภาษาไทย |
 Mi-24 Hind | ||
| The Mil Mi-24 helicopter is developed by Mil bureau from the year 1960 and manufactured at Arsenyev and Rostov plants known as Hind.
The Mil Mi-24 helicopter that would be able to airlift armed troops while having speed and armor to survive enemy fire as well as sufficient armament to suppress
ground defences. The Mi-24 features large wings that not only provide attachments for a variety of weapons but also provide much of the lift in forward flight.
The five-blades main rotor is mounted on the top of fuselage mid-section, while short, stub, weapon-carrying wings are mounted at the fuselage mid-section.
Two turboshaft engines are mounted above body mid-section with two round air intakes located just above the cockpit and exhaust ports on the sides of engines.
Each stub wing has three hardpoints for total of six stations. The aircraft consists of Armored cockpits and titanium rotor head able to withstand 20-mm cannon hits.
The aircraft can store an additional ammunition in the compartment in lieu of carrying troops. The first flight flew on September 19,1969 and by late of year 1990
more than 2500 Mi-24 and variants were built. Variants: * Mi-24 Hind-A: First production model with tail rotor on the port side, used in assualt role with room for three crew and eight armed troops, and most upgraded to Hind-D or Hind-E. * Mi-24 Hind-C: Trainer version similar to late production of Hind-A but lacking gun turret and wing tip hardpoints. * Mi-24D Hind-D: Dedicated assault gunship with new forward fuselage featuring seperate cockpits for pilot and gunner, new gun turret installation, bullet proof windscreens, and improved armor with rotor head and rotor blades can withatand 20 mm. gun, four anti-tank missiles on two wingtip stations. * Mi-24V Hind-E: Improved gun ship similar to Mi-24D but armed with AT-6 anti-tank missiles and AA-8 air-to-air missiles. * Mi-24P Hind-F: Similar to Hind-E but 12.7 mm. cannon replaced by large 30 mm cannon and mounted to the side of fuselage. Empty weight to 8,200 kg. while boosting maximum gross weight to 12,000 kg. * Mi-25: Export version of the Hind-D * Mi-35: Export version of the Hind-E. The Mi-35M has a twin barrel 23-mm.gun. * Mi-35P: Export version of the Hind-F | ||
| SPECIFICATIONS Mi-24D Hind-D | ||
| Power Plant (Turboshaft) | Isotov | TV-3-117 |
| Number of Engine | 2 | |
| Engine Power | 2,200 shp.each | |
| Length of fuselage | 17.50 m | |
| Length include Main Rotor | 21.6 m. | |
| Main Rotor Diameter | Five Blades Rotor | 17.3 m. |
| Tail Rotor Diameter | three blades | 3.9 m |
| Max. Speed | 168 mph (335 km/h) | |
| Empty Weight | 8,500 kgs | |
| Max Takeoff Weight | 11,100 kgs | |
| Max. Fuel (internal) | 1,840 litres | |
| Range | 450 km. (normal load) | |
| Crew | 2 (pilot & weapon officer) | |
| Armament | one 12.7 mm. cannon (hind-D) or one 30 mm. cannon (hind-F) |
air-to-air Missile R-60/AA-8 Aphid air-to-surface missile up to four AT-2 or AT-3 anti-tank missile |
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cockpit Mi-24 Hind Gunner Panel | |
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cockpit Mi-24 Hind,Pilot Panel | |
| 1 nm.(nautical mile) = 1.15155 miles, 1 kt (knot) = 1.15155 mile / hr. 1 mach = 761 mph.(SL,ISA) |
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