Mil Mi-14
Twin-Turboshaft Multi-Purpose Maritime Helicopter
Technical Data
Powerplants: Two Kilmov (Isotov) TV3-117MT turboshafts
Developing: 1,454kW (1,950shp)
Driving: Five-blade main and three-blade tail rotors
Main rotor diameter: 21.29m (69ft 10.25in)
Fuselage length: 18.38m (60ft 3.25in)
Height: 6.93m (22ft 9in)
All-up weight: 14,000kg (30,865lb)
Maximum speed: 230km/h (143mph)
Cruise speed: 215km/h (133mph)
Operational ceiling: 13,125ft
Maximum range: 1,135km (705miles)
Endurance: 5hr 56min
Accommodation: Four crew
Warload: Includes torpedoes, nuclear depth bombs and depth charges in an enclosed weapons bay in the lower hull
First flown: September 1969 (V-14 prototype); 1973 (Mi-14PL)
Entered service: 11 May 1976
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60¿©´ëÀÇ Mi-14 Haze°¡ ¿©ÀüÈ÷ ·¯½Ã¾ÆÇرº¿¡¼ ¿î¿ëÁßÀ̸ç
(10´ëÀÇ Mi-14PL°ú ¼ö´ëÀÇ Mi-14PSµµ Æ÷ÇԵ˴ϴÙ)
ºÒ°¡¸®¾Æ, Äí¹Ù, ¿¡µð¿ÀÇǾÆ, ºÏÇÑ, ¸®ºñ¾Æ, ·ç¸¶´Ï¾Æ, ±×¸®°í ½Ã¸®¾Æ¿¡¼ Mi-14PLÀ» ¿î¿ëÁßÀÔ´Ï´Ù.
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(ÀÌ ±âü´Â Æú¶õµå¿¡¼´Â Mi-14PW¶õ Á¦½Ä¸íÀ» °¡Áö°í ÀÖ½À´Ï´Ù)
ÀÌ Mi-14PLÀº Kh-23 (AS-7 'Kerry')°ø´ëÁö ¹Ì»çÀÏÀ» ¿î¿ëÇÏ´Â Mi-14PL 'Strike'¹öÁ¯°ú ´õ¿í Çâ»óµÈ Àڱ⺯Ȱ¨Áö±â¿Í ±¸Á¶¿ë Å°Æ®°¡ Ãß°¡µÈ Mi-14PLMÀ¸·Î °³·®µÇ¾îÁý´Ï´Ù.
¼Ò¼öÀÇ Mi-14BT 'Haze-B'´Â ¼ÒÇØÇï±â¹öÁ¯À̸ç Mi-14PS 'Haze-C'´Â ¼ö»ö/±¸Á¶¿ë Çï±â·Î ÃÖ´ë 19¸íÀ» ¼ö¿ëÇÒ¼ö ÀÖ½À´Ï´Ù.
¸¶Áö¸·À¸·Î Æú¶õµåÇرºÀº ÇÑ´ëÀÇ Mi-14PW¸¦ Mi-14PX·Î °³¼öÇÏ°í ASWÀåºñ¸¦ Á¦°ÅÇÑ ¼ö»ö/±¸Á¶¿ë ÈƷñâ·Î »ç¿ëÇÏ°í ÀÖ½À´Ï´Ù.
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