| LTS101 / LTP101 | |
|---|---|
| |
| LTS101-750C engine installation (left engine) in a Bell 222UT | |
| Type | Turboprop / turboshaft |
| National origin | United States |
| Manufacturer | Lycoming Engines Honeywell Aerospace |
| First run | 1960 |
| Major applications | Aérospatiale HH-65 Dolphin Air MBB/Kawasaki BK117 Bell 222 Eurocopter AS350 AStar |
The Lycoming (now Honeywell) LTS101 is a turboshaft engine family ranging from 650 to 850 shaft horsepower, used in a number of popular helicopters,[1] and, as the LTP101 turboprop, light aircraft. Both models carry the US military designation T702. The engine was originally designed at the Lycoming Turbine Engine DivisioninStratford, Connecticut, but is now produced by Honeywell Aerospace.
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Data from [2]
Related development
Comparable engines
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| Opposed piston engines |
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| Radial engines and H engines |
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| Aircraft diesel engines |
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| Turbofans |
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| Turboprops/Turboshafts |
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| Aero-derivative marine gas turbines |
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| Joint development | Avco (Lycoming)/Pratt & Whitney: T800-APW (Turboshaft) |
| See also |
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| Turboprops/Turboshafts |
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| Turbofans |
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| Joint development |
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Note: AVCO Lycoming/Textron Lycoming engines marked with * | |||||||||||
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United States military gas turbine aircraft engine designation system
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| Turbojets |
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| Turboprops/ Turboshafts |
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| Turbofans |
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| Adaptive cycle engines |
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