Mil Mi-60 MAI

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Mi-60 MAI
Role Light utility helicopterTemplate:Short description
National origin Russia
Manufacturer Mil
Designer Marat Nikolayevich Tishchenko[1][2]
Status Unrealised project

The Mil Mi-60 MAI (Cyrillic: Миль Ми-60 МАИ) was a joint project between Mil and the Moscow Aviation Institute to develop a light utility helicopter.[3] A mockup was displayed at the MAKS 2001 air show,[2][3][4] where Russian aerospace journal Aviatsiya i Kosmonavtika (Авиация и космонавтика; "Aviation and Space") described it as a "little brother" to the Mil Mi-34.[5]

The Mi-60 MAI was intended to fulfil a range of general aviation activities, including pilot training, agricultural work, police and firefighting duties, resource monitoring, aerial photography, and tourism.[2] Domestic demand in Russia for such an aircraft was estimated at around 400–600 units.[2] No Russian manufacturer was producing a lightweight helicopter such as this, and foreign aircraft were unsuitable for Russian conditions.[6]

The design was further presented at the 1997 International Aviation Forum in Moscow, and the World Salon of Inventions in Brussels the same year.[7] It won a gold medal at the latter event.[7]

Design

The Mi-60 MAI was a conventional design for a light helicopter, with a pod-and-boom fuselage, a three-bladed main rotor, two-bladed tail rotor, and a skid undercarriage with rear wheels on each skid.[3][4][2] The pilot and a single passenger were to sit side-by-side in an extensively-glazed, enclosed cabin with dual controls.[1]

At different stages of development, a variety of powerplants were proposed, including:

These were to be located inside the fuselage, behind the cabin, with power transmitted to the rotor through V-belts.[1] In the twin-engine versions, the engines were to be located side-by-side.[1][4] One criterion for engine selection was favouring engines that could run on automotive-grade petrol.[2][6] This would allow the aircraft to operate in regions with less well-developed infrastructure.[8] The twin-engine variants were expected to be able to continue to fly on only one engine.[7]

Construction was to make extensive use of composite materials.[6]

Development

Initial funding for the project came from the Russian Ministry of Education.[3] Development started in 1993 and technical work was finished the following year.[3] In 1997, the Russian Army became a sponsor, hoping to use the Mi-60 MAI as a helicopter trainer.[3]

Construction of a mockup commenced at the Kazan helicopter factory in 2000.[3] It was displayed the following year at the MAKS air show, and production was planned to start the same year.[3] Production would have taken place at the Rostvertol factory in Rostov-on-Don[4] As of 1998, an estimated $30 million was still required to put the aircraft into production.[7]

Development work on the program ended in 2001,[2] although it was still included in the Russian federal aviation plan for 2002–10.[3] As of 2013, no examples had been constructed.[4]

Specifications (as designed, with VAZ engine)

Template:Aircraft specs

Notes

References

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  1. a b c d e f Mikheev 1998, p.268
  2. a b c d e f g Mikheev 2007, p.318
  3. a b c d e f g h i j k l m Jackson 2007, p.497
  4. a b c d e f g h Gordon & Komissarov 2013, p.606
  5. Nikolskiy 2001, p.9
  6. a b c MAI+Mil new ultralight, p.16
  7. a b c d MAI+Mil new ultralight, p.19
  8. MAI+Mil new ultralight, p.17

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Bibliography

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External links

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