Mil Mi-1T
A modification of the Mil Mi-1, the Mi-1T served as a transport helicopter. The aircraft holds the pilot and 2 passengers and is eqipped with the AI-26V radial engine.
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 1
Crew seating: Single seater
Landing gear: Wheels (non-retractable)
Layout and Dimensions
Data on aircraft size| Overall Dimensions | ||
|---|---|---|
| Overall Height: | ||
| Overall Length: | ||
| Overall Width: | 14.30 m | 46.9 ft |
| Airframe Dimensions | ||
|---|---|---|
| Airframe Length: | ||
| Airframe Width: | ||
| Airframe Height: | ||
| Landing Gear Dimensions | ||
|---|---|---|
| Landing Gear Base: | ||
| Landing Gear Track: | ||
| Cabin Dimensions | ||
|---|---|---|
| Cabin Internal Height: | ||
| Cabin Internal Length: | ||
| Cabin Internal Width: | ||
Weights and Performance
Data on aircraft weight and flight characteristics| Weights | ||
|---|---|---|
| Max Gross Weight (ground): | 2,300 kg | 5,071 lb |
| Max Gross Weight (airborne): | ||
| Max Take-off Weight: | 2,300 kg | 5,071 lb |
| Empty Weight: | 1,796 kg | 3,959 lb |
| Useful Load: | 504 kg | 1,111 lb |
| Empty Weight Fraction: | 0.781 | |
| Climb Performance | ||
|---|---|---|
| Max Rate of Climb: | ||
| Hover Performance | ||
|---|---|---|
| Hover Ceiling IGE: | 2,700 m | 8,858 ft |
| Hover Ceiling OGE: | ||
| Limitations | ||
|---|---|---|
| Max Level Flight Speed: | 175 km/h | 94 kts |
| Never Exceed Speed: | ||
| Service Ceiling: | 3,500 m | 11,483 ft |
| Range and Endurance | ||
|---|---|---|
| Max Range: | 380 km | 205 nm |
| Max Endurance: | ||
Engine Details
Aircraft powerplant (lift and/or propulsion)Provided powerplant data is for uninstalled, sea level, static operations.
| Powerplant | ||
|---|---|---|
| Number of engines: | 1 | |
| Designation: | Ivchenko AI-26V reciprocating | |
| Manufacturer: | Ivchenko | |
| Normal Ratings | ||
|---|---|---|
| Max continuous: | ||
| Take-off / rated: | 429 kW | 575 hp |
| Intermediate: | ||
| Maximum: | ||
| OEI Ratings | ||
|---|---|---|
| OEI contingency: | ||
| OEI continuous: | ||
| OEI 30-second: | ||
| OEI intermediate: | ||
Primary Lift Device
Data on primary lift devices such as main rotors| Main Rotor Characteristics | ||
|---|---|---|
| Diameter: | 14.30 m | 46.92 ft |
| RPM: | ||
| Direction of Rotation: | Clockwise | |
| Hub Type: | ||
| Main Rotor Blade Characteristics | ||
|---|---|---|
| Blade Construction: | ||
| Blade Chord: | ||
| Blade Tip Geometry: | Conventional | |
| Blade Twist: | ||
| Number of Blades: | 3 | |
| Main Rotor Derived Characteristics | ||
|---|---|---|
| Disc Area: | 160.61 m² | 1728.8 ft² |
| Disc Loading: | 14.32 kg/m² | 2.933 lb/ft² |
| Solidity: | ||
| Main Rotor Blade Derived Characteristics | ||
|---|---|---|
| Blade area per blade: | ||
| Tip Speed: | ||
Primary Control Device
Data on primary control devices such as tail rotors| Tail Rotor Characteristics | ||
|---|---|---|
| Diameter: | ||
| Configuration: | Pusher | |
| Direction of Rotation: | Top blade aft | |
| RPM: | ||
| Tail Rotor Blade Characteristics | ||
|---|---|---|
| Number of Blades: | 3 | |
| Blade Construction: | ||
| Blade Chord: | ||
| Blade Twist: | ||
| Tail Rotor Derived Characteristics | ||
|---|---|---|
| Disc Area: | ||
| Solidity: | ||
| Tail Rotor Blade Derived Characteristics | ||
|---|---|---|
| Tip Speed: | ||
| Blade Area (per blade): | ||
Related VFS Resources
Resources related to the Mi-1T , provided by the Vertical Flight Society.Forum Proceedings
Vertiflite articles
Enter a search term in the box above.
Web files from vtol.org
Enter a search term in the box above.
Webpages from vtol.org
Enter a search term in the box above.
Related Public Resources
Resources related to the Mi-1T , provided by public sources across the internet.Publicly-funded resources provided by the US Government
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
Public resources provided by select scholarly and academic sources
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
Enter a search term in the box above.
