Editor -- pointing to
http://www.globalaircraft.org/planes/mi-6_hook.pl
Format:
HTML
|
Text Only
Word wrap:
Off
| On
<!--BEGIN SPECIFICATIONS--> Mi-6 Hook Specifications Primary Function: Heavy transport helicopter Contractor: Mil Crew: Five - two pilots, flight engineer, navigator, and radio operator Unit Cost: N/A Powerplant Two 5425shp (4045kW) Soloviev D-25V turboshafts, driving a five blade main rotor and four blade tail rotor -- (Mi-6T) Dimensions Fuselage Length: 108 ft, 11 in (33.18 m) -- excluding nose gun Rotor Diameter: 114 ft, 10 in (35 m) Height: 32 ft, 4 in (9.86m) Weights Empty: 60,055lb (27,240kg) -- (Mi-6T) Maximum Takeoff: 93,700lb (42,500kg) -- (Mi-6T) Performance Speed: 135kt (250km/h / 158 mph) -- (Mi-6T) Ceiling: 14,750ft -- (Mi-6T) Range: 780nm (1450km) -- (Mi-6T w/ aux. fuel) Armament Some Mi-6 helos are fitted with a 12.7mm machine gun on the aircraft's nose <!--END SPECIFICATIONS--> <!--BEGIN ACHIEVEMENTS--> Mi-6 Hook Achievements When first flown in 1957, the Mi-6 Hook was the world's largest rotary-wing aircraft. <!--END ACHIEVEMENTS--> <!--BEGIN FEATURES--> <!-- Mi-6 Hook Features --> <!--END FEATURES--> <!--BEGIN BACKGROUND--> <!-- Mi-6 Hook Background --> <!--END BACKGROUND-->
Please note that your edits are only suggestions for changes and will
not
appear on the website unless approved by the webmaster!