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SZD-36 Cobra
|
SZD-36 Cobra. |
| Type designation |
SZD-36 |
| Competition class |
Club, formerly Standard |
| Number built |
800 |
| Crew |
1 |
| Length |
7.05 m |
| Height |
1.59 |
| Cockpit width |
|
| Cockpit height |
|
| Wingspan |
15 m |
| Wing area |
11.6 m² |
| Aspect ratio |
19.2 |
| Wing profile |
FX-61-168/60-1261 |
| Empty mass |
ca. 275 kg |
| Maximum mass |
405 kg |
| Wing loading |
ca. 32 kg/m² |
| Maximum speed |
250 km/h (135 kts) |
| Rough air speed |
140 km/h (75.5 kts) |
| Stall speed |
60 km/h (32.5 kts) |
| Minimum sink rate |
ca. 0.7 m/s |
| Best glide ratio |
38 |
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.
|
The single-seat SZD-36 Cobra was designed by Okarmus and Mynarski for the 1970 World championships. It is based on the previous model Foka 5 but with but with retractable wheel and a laminar airflow producing 38:1 best L/D. The plane placed 2nd and 3rd in the World Championships. The Cobra was built very strong and is still used as an aerobatic demonstration plane.
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