Mi-1 HARE
The Mi-1 Hare entered series production in 1951. The Mi-1 remained in production until 1964. Poland built a version designated SM-1. The three-blade main rotor is mounted on a high hump on top of the fuselage midsection. The single radial piston engine is mounted beneath a hump on top of cabin. The fuselage, which is tadpole-shaped when viewed from bottom, features a rounded nose and rear sections with a stepped, glassed-in cockpit and a long, thin, tapered tail boom. The tail consists of a swept-back fin with a rotor on the right top. Small flats are equally tapered and mounted directly in front of the fin.
Specifications
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| Country of Origin | Russia
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| Builder | MIL
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| Role | Utility, liaison
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| Similar Aircraft | None
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| Rotor diameter | 47 ft (14.36 m)
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| Length | 39 ft, 8 in (12.2 m)
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| Height |
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| Weight |
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| Engine |
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| Maximum speed |
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| Cruising speed |
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| Range |
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| Service Ceiling |
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| Armament | Usually none
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| Crew | One
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| Cost |
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| User Countries |
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Sources and Resources
http://www.fas.org/man/dod-101/sys/ac/row/mi-1.htm
Maintained by Robert Sherman
Originally created by John Pike
Updated Tuesday, September 21, 1999 10:18:15 AM
