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.
VTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 1
Crew seating: Single seater
Landing gear: Wheels (non-retractable)
Overall Dimensions | ||
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Overall Height: | ||
Overall Length: | ||
Overall Width: | 14.30 m | 46.9 ft |
Airframe Dimensions | ||
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Airframe Length: | ||
Airframe Width: | ||
Airframe Height: |
Landing Gear Dimensions | ||
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Landing Gear Base: | ||
Landing Gear Track: |
Cabin Dimensions | ||
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Cabin Internal Height: | ||
Cabin Internal Length: | ||
Cabin Internal Width: |
Weights | ||
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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 | ||
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Max Rate of Climb: |
Hover Performance | ||
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Hover Ceiling IGE: | 2,700 m | 8,858 ft |
Hover Ceiling OGE: |
Limitations | ||
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Max Level Flight Speed: | 175 km/h | 94 kts |
Never Exceed Speed: | ||
Service Ceiling: | 3,500 m | 11,483 ft |
Range and Endurance | ||
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Max Range: | 380 km | 205 nm |
Max Endurance: |
Provided powerplant data is for uninstalled, sea level, static operations.
Powerplant | ||
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Number of engines: | 1 | |
Designation: | Ivchenko AI-26V reciprocating | |
Manufacturer: | Ivchenko |
Normal Ratings | ||
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Max continuous: | ||
Take-off / rated: | 429 kW | 575 hp |
Intermediate: | ||
Maximum: |
OEI Ratings | ||
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OEI contingency: | ||
OEI continuous: | ||
OEI 30-second: | ||
OEI intermediate: |
Main Rotor Characteristics | ||
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Diameter: | 14.30 m | 46.92 ft |
RPM: | ||
Direction of Rotation: | Clockwise | |
Hub Type: |
Main Rotor Blade Characteristics | ||
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Blade Construction: | ||
Blade Chord: | ||
Blade Tip Geometry: | Conventional | |
Blade Twist: | ||
Number of Blades: | 3 |
Main Rotor Derived Characteristics | ||
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Disc Area: | 160.61 m² | 1728.8 ft² |
Disc Loading: | 14.32 kg/m² | 2.933 lb/ft² |
Solidity: |
Main Rotor Blade Derived Characteristics | ||
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Blade area per blade: | ||
Tip Speed: |
Tail Rotor Characteristics | ||
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Diameter: | ||
Configuration: | Pusher | |
Direction of Rotation: | Top blade aft | |
RPM: |
Tail Rotor Blade Characteristics | ||
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Number of Blades: | 3 | |
Blade Construction: | ||
Blade Chord: | ||
Blade Twist: |
Tail Rotor Derived Characteristics | ||
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Disc Area: | ||
Solidity: |
Tail Rotor Blade Derived Characteristics | ||
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Tip Speed: | ||
Blade Area (per blade): |