Attribute | Curtiss P-36 Hawk × | North American T-28 Trojan × |
---|---|---|
General | ||
Manufacturer | Curtiss | North American Aviation NAA |
Model | Curtiss P-36 Hawk | North American T-28 Trojan |
Country | United States | United States |
Manufactured from (year) | 1938 | 1950 |
Manufactured to (year) | 1944 | 1957 |
Type | Military Propellor Planes | Military Trainers |
1↑Icao | P36 | T28 |
Performance | ||
Engine | 1x Pratt & Whitney R-1830-17 Twin Wasp | 1x Wright R-1820-86 Cyclone |
Power, hp (hp) | 1,050 | 1,425 |
Max cruise speed (km/h) | 504 | 556 |
Approach speed (km/h) | 120 | 115 |
Travel range (km) | 1,389 | 1,704 |
Service ceiling (m) | 10,058 | 10,820 |
Rate of climb (m/sec) | 17.27 | 17.98 |
Take off distance (m) | - | 400 |
Landing distance (m) | - | 400 |
Weights | ||
Max take off weight (kg) | 2,726 | 3,856 |
Max landing weight (kg) | 2,563 | 3,542 |
Max payload (kg) | 550 | 600 |
Fuel tank capacity (l) | 511 | 674 |
Dimensions | ||
Seats | 1 | 2 |
Exterior length (m) | 8.7 | 10.4 |
Tail height (m) | 2.84 | 3.86 |
Fuselage diameter (m) | 1.2 | 1.6 |
Wing span (m) | 11.38 | 12.3 |
Wing tips | No Winglets | No Winglets |