| 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 |