Mil Mi-60 MAI
| Mi-60 MAI | |
|---|---|
| Role | Light utility helicopter |
| 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:
- one 120-kilowatt (160 hp) Lycoming O-320-B2C piston engine[1][4]
- one 150-kilowatt (200 hp) Aviadvigatel D-150 wankel engine[1][4]
- one 145-kilowatt (194 hp) Textron Lycoming HIO-360-F1AD piston engine[3]
- one 177-kilowatt (237 hp) VAZ-426 wankel engine[3]
- two 84.6-kilowatt (113.5 hp) Rotax 914F piston engines.[3][4]
- two 103-kilowatt (138 hp) LOM M332A piston engines[3]
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)
Data from Jackson 2007, p.497, except as noted.
General characteristics
- Crew: one pilot
- Capacity: 1 passenger
- Length: 7.370 m (24 ft 2 in) (fuselage, including tail rotor)[8]
- Height: 2.286 m (7 ft 6 in) [8]
- Max takeoff weight: 1,300 kg (2,866 lb)
- Powerplant: 1 × VAZ-426 piston engine, 177 kW (237 hp)
- Main rotor diameter: 10.00 m (32 ft 10 in)
Performance
- Maximum speed: 225 km/h (140 mph, 121 kn)
- Cruise speed: 185 km/h (115 mph, 100 kn)
- Range: 400 km (250 mi, 220 nmi)
- Service ceiling: 5,500 m (18,000 ft)
- Rate of climb: 142 m/s (28,000 ft/min)
Notes
References
- ↑ 1.0 1.1 1.2 1.3 1.4 1.5 Mikheev 1998, p.268
- ↑ 2.0 2.1 2.2 2.3 2.4 2.5 2.6 Mikheev 2007, p.318
- ↑ 3.00 3.01 3.02 3.03 3.04 3.05 3.06 3.07 3.08 3.09 3.10 3.11 3.12 Jackson 2007, p.497
- ↑ 4.0 4.1 4.2 4.3 4.4 4.5 4.6 4.7 Gordon & Komissarov 2013, p.606
- ↑ Nikolskiy 2001, p.9
- ↑ 6.0 6.1 6.2 MAI+Mil new ultralight, p.16
- ↑ 7.0 7.1 7.2 7.3 MAI+Mil new ultralight, p.19
- ↑ 8.0 8.1 8.2 MAI+Mil new ultralight, p.17
Bibliography
- "МАИ+Миль новый сверхлегкий" [MAI+Mil new ultralight]. Вертолёт. No. 2. Kazan: Omega Research Centre. 1998. pp. 16–19.
- Mikheev, Vadim Rostislavovich (1998). МВЗ им. М. Л. Миля 50 лет [The Moscow Helicopter Plant named for M. L. Mil turns 50]. Moscow: Lyubimaya.
- Mikheev, Vadim Rostislavovich (2007). МВЗ имени М. Л. Миля [The Moscow Helicopter Plant named for M. L. Mil]. Moscow: Polygon.
- Nikolskiy, Mikhail (2001). "Первый российский авиасалон XXI бека" [The First Russian Air Show of the 21st Century]. Авиация и космонавтика. No. 9. Moscow: Techinform. pp. 1–10.
- Gordon, Yefim; Komissarov, Sergey (2013). Unflown Wings: Soviet and Russian Unrealised Aircraft Projects 1925-2010. Manchester: Créey Publishing.
- Jackson, Paul, ed. (2007). Jane's All the World's Aircraft 2007-08 (98th ed.). London: Jane's Publishing Group.