Mil Mi-10

1. Mil Mi-10 · Wikipedia revision 1369755882 ↗

   Type

   Infobox · Type

   Aerial crane

   National origin

   Infobox · National origin

   Russia

   Manufacturer

   Infobox · Manufacturer

   Mil Moscow Helicopter Plant

   Status

   Infobox · Status

   Active as of 2014 (Mi-10K)

   Number built

   Infobox · Number built

   55

   Manufactured

   Infobox · Manufactured

   1964–69

   Introduction date

   Infobox · Introduction date

   1963

   First flight

   Infobox · First flight

   15 June 1960

   Developed from

   Infobox · Developed from

   Mil Mi-6

   Crew

   Specifications (Mi-10) · Crew

   3 (pilot, copilot and flight engineer, navigator/radio operator and optional technician)

   Capacity

   Specifications (Mi-10) · Capacity

   28 passengers or 3 t (3,000 kg; 6,600 lb) internally up to 15 t (15,000 kg; 33,000 lb) payload on platform or 8 t (8,000 kg; 18,000 lb) max slung payload

   Length

   Specifications (Mi-10) · Length

   32.86 m (107 ft 10 in) (fuselage only), 41.89 m (137 ft 5 in) (overall length, rotors turning)

   Empty weight

   Specifications (Mi-10) · Empty weight

   27,100 kg (59,745 lb) , Mi-10K 25,450 kg (56,110 lb)

   Gross weight

   Specifications (Mi-10) · Gross weight

   43,550 kg (96,011 lb) , Mi-10K 37,000 kg (82,000 lb)

   Max takeoff weight

   Specifications (Mi-10) · Max takeoff weight

   43,700 kg (96,342 lb) , Mi-10K 38,000 kg (84,000 lb)

   Powerplant

   Specifications (Mi-10) · Powerplant

   2 × Soloviev D-25V turboshaft, 4,100 kW (5,500 hp) each

   Main rotor diameter

   Specifications (Mi-10) · Main rotor diameter

   35.00 m (114 ft 10 in)

   Maximum speed

   Specifications (Mi-10) · Maximum speed

   335 km/h (208 mph, 181 kn)

   Cruise speed

   Specifications (Mi-10) · Cruise speed

   180 km/h (110 mph, 97 kn)

   Range

   Specifications (Mi-10) · Range

   430 km (270 mi, 230 nmi)

   Ground clearance under fuselage

   Specifications (Mi-10) · Ground clearance under fuselage

   3.75 m (12 ft 4 in)

   Main rotor area

   Specifications (Mi-10) · Main rotor area

   962 m 2 (10,350 sq ft)

   Hovering ceiling out of ground effect

   Specifications (Mi-10) · Hovering ceiling out of ground effect

   3,000 m (9,840 ft)

2. Wikipedia contributors ↗

   Height

   Лётно-технические характеристики · Высота

   Высота : 9,9 м (с остановленным хвостовым винтом)

   Service ceiling

   Лётно-технические характеристики · Практический потолок

   Практический потолок : 3000 м

Reference text from Wikipedia contributors, used under CC BY-SA 4.0.