Attribute | Curtiss-Wright Junior × | Yakovlev Yak-55 × |
---|---|---|
General | ||
Manufacturer | Curtiss | Yakovlev |
Model | Curtiss-Wright Junior | Yakovlev Yak-55 |
Country | United States | Russia |
Manufactured from (year) | 1930 | 1981 |
Manufactured to (year) | 1932 | 1993 |
Type | Private Single Engine | Aerobatic |
Icao | CW1 | YK55 |
Performance | ||
Engine | 1x Szekely SR-3 | 1x Vedeneyev M14P 9-cylinder radial engine |
Power, hp (hp) | 45 | 360 |
Max cruise speed (km/h) | 130 | 306 |
Approach speed (km/h) | 48 | 100 |
Travel range (km) | 315 | 706 |
1↑Service ceiling (m) | 3,658 | 4,000 |
Rate of climb (m/sec) | 3.05 | 15.49 |
Take off distance (m) | 61 | 150 |
Landing distance (m) | 76 | 300 |
Weights | ||
Max take off weight (kg) | 442 | 975 |
Max payload (kg) | 145 | 90 |
Fuel tank capacity (l) | 35 | 276 |
Dimensions | ||
Seats | 2 | 1 |
Exterior length (m) | 6.5 | 7.29 |
Tail height (m) | - | 2.25 |
Fuselage diameter (m) | 0.8 | 1 |
Wing span (m) | 12.04 | 8.15 |
Wing tips | No Winglets | No Winglets |