Attribute | ![]() Hawker 400XP × | ![]() Lockheed P-80 Shooting Star × |
---|---|---|
General | ||
Manufacturer | Hawker Beechcraft | Lockheed Martin Aeronautics |
Model | Hawker 400XP | Lockheed P-80 Shooting Star |
Country | United States | United States |
Manufactured from (year) | 2003 | 1945 |
Manufactured to (year) | 2009 | 1950 |
Type | Light Business Jets | Fighter Jets |
Icao | BE40 | P80 |
Performance | ||
Engine | 2x 2 X Pratt and Whitney JT15D-5 | 1x Allison J33-A-35 |
Power, lbf (lbf) | 2,965 | 4,600 |
Avionics | Collins Pro Line 4, Collins DBU-5000 Data Base Unit, Honeywell Mark V TAWS | - |
Max cruise speed (km/h) | 833 | 956 |
Approach speed (km/h) | 220 | - |
Travel range (km) | 2,898 | 2,222 |
Fuel economy (km/l) | 1.047 | - |
Service ceiling (m) | 13,716 | 14,265 |
Rate of climb (m/sec) | 20.42 | 34.9 |
Take off distance (m) | 1,432 | - |
Landing distance (m) | 918 | - |
Weights | ||
Max take off weight (kg) | 7,393 | 7,257 |
Max landing weight (kg) | 7,121 | 6,350 |
Max payload (kg) | 914 | 1,000 |
Fuel tank capacity (l) | 2,775 | 3,350 |
Baggage volume (m³) | 1 | - |
Dimensions | ||
Seats | 8 | 1 |
Cabin height (m) | 1.47 | - |
Cabin width (m) | 1.5 | - |
Cabin length (m) | 4.78 | - |
Exterior length (m) | 14.76 | 10.5 |
Tail height (m) | 4.1 | 3.45 |
Fuselage diameter (m) | 1.7 | 1 |
Wing span (m) | 13.23 | 11.83 |
Wing tips | No Winglets | No Winglets |