| Manufacturer |
OKB Laros |
Wolf Hirth |
| Description |
The Laros-100 is a Russian light aircraft specifically designed for aerobatics flying. |
The Hirth Hi 27 Acrostar was designed by Arnold Wagner to win aerobatic competitions, in part by having handling independent of orientation, upright or inverted. |
| ICAO Code |
|
HI27 |
| First Flight |
2013-06-14 |
1970-04-16 |
| Designer |
Vladimir P. Lapshin |
Arnold Wagner |
| Length (m) |
6.45 |
6.11 |
| Height (m) |
1.85 |
2.5 |
| Cockpit Crew |
|
1 |
| Max Speed (km/h) |
260 |
305 |
| Cruise Speed (km/h) |
|
252 |
| Min Speed (km/h) |
85 |
96 |
| Max Ceiling (m) |
|
7500 |
| Rate of Climb (m/s) |
7 |
15 |
| National Origin |
Russia |
West Germany |
| Number Built |
1 |
10 |
| Powerplant Description |
1 × Lycoming AEIO-360 air-cooled, fuel injection flat-four engine, 149 kW (200 hp) each |
1 × Franklin 6A-350-C1 6-cylinder horizontally opposed piston engine, 164 kW (220 hp) each |
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Laros-100 |
en.wikipedia.org/wiki/Hirth_Acrostar |
| Flat Wing Span (m) |
7.15 |
8 |
| Flat Wing Area (m²) |
10.7 |
10.6 |
| Flat Wing Aspect Ratio |
5 |
6.03 |
| Wake Category |
|
L |
| Number of Engines |
1 |
1 |