Flat Wing Aspect Ratio
5.4
Maximum Take-Off Weight
0.258 t (paragliders: kg)
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
|
Latécoère 225 |
0.258 |
23 |
Similar airplanes
All data (21 fields)
- Name
- Latécoère 225
- Manufacturer
- Latécoère
- Description
- The Latécoère 225 was an unusual single seat canard microlight amphibian, with a swept wing, and of pusher configuration.
- First Flight
- 1984-07-18
- Designer
- Nono Larsen
- Length (m)
- 4.95
- Height (m)
- 2.15
- Cockpit Crew
- 1
- Max Speed (km/h)
- 120
- Cruise Speed (km/h)
- 85
- Min Speed (km/h)
- 45
- Rate of Climb (m/s)
- 2.7
- National Origin
- France
- Number Built
- 1
- Powerplant Description
- 1 × JPX PUL 425 twin cylinder, horizontally opposed, air-cooled two-stroke, 18 kW (24 hp) each
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lat%C3%A9co%C3%A8re_225
- Flat Wing Span (m)
- 8.03
- Flat Wing Area (m²)
- 11.85
- Flat Wing Aspect Ratio
- 5.4
- Aircraft Engine
- JPX PUL 425
- Number of Engines
- 1