Laros-100

ยท OKB Laros
Length
6.45 m
Flat Wing Span
7.15 m
Height
1.85 m
Flat Wing Area
10.7 m²
Flat Wing Aspect Ratio
5
Max Speed
260 km/h
Number of Engines
1
First Flight
2013-06-14
Number Built
1
Maximum Take-Off Weight
0.7 t (paragliders: kg)
Total Fuel Capacity
100

Pictures

No pictures yet for this family.

Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg)) Total Fuel Capacity
Laros-100 0.7 100

Similar airplanes

Name Aircraft Engine Length (m) Flat Wing Span (m) Max Seating
Eagle Aircraft Eagle 150 6.45 7.16 Compare
Jurca Sirocco Lycoming O-235 6.15 7 1 Compare
Aviatika-900 Acrobat 5.7 7.15 Compare
Ganzavia GAK-22 Dinó Lycoming O-235 6.1 7.7 Compare
Grumman American AA-1 Lycoming O-235 5.87 7.46 Compare
Hirth Acrostar 6.11 8 Compare
All data (18 fields)
Name
Laros-100
Manufacturer
OKB Laros
Description
The Laros-100 is a Russian light aircraft specifically designed for aerobatics flying.
First Flight
2013-06-14
Designer
Vladimir P. Lapshin
Length (m)
6.45
Height (m)
1.85
Max Speed (km/h)
260
Min Speed (km/h)
85
Rate of Climb (m/s)
7
National Origin
Russia
Number Built
1
Powerplant Description
1 × Lycoming AEIO-360 air-cooled, fuel injection flat-four engine, 149 kW (200 hp) each
Wikipedia Article (URL)
en.wikipedia.org/wiki/Laros-100
Flat Wing Span (m)
7.15
Flat Wing Area (m²)
10.7
Flat Wing Aspect Ratio
5
Number of Engines
1