Northrop T-38 Talon [+]Compare [E]dit [H]istory
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Object «Northrop T-38 Talon» has attributes [Show empty attributes][Hide empty attributes]
| Attribute | Value |
|---|---|
| General | |
| Manufacturer | Northrop Grumman |
| Model | Northrop T-38 Talon |
| Country | United States |
| Manufactured from | 1961 year |
| Manufactured to | 1972 year |
| Type | Military Trainers |
| Icao | T38 |
| Performance | |
| Engine | 2x General Electric J85-5A |
| Power, hp | Add |
| Power, lbf | 3,850 lbf |
| Avionics | Add |
| Max cruise speed | 1,380 km/h |
| Approach speed | 246 km/h |
| Travel range | 1,835 km |
| Fuel economy | 0.827 km/l |
| Service ceiling | 15,240 m |
| Rate of climb | 170.69 m/sec |
| Take off distance | 1,128 m |
| Landing distance | 1,372 m |
| Weights | |
| Max take off weight | 5,670 kg |
| Max landing weight | Add |
| Max payload | 630 kg |
| Fuel tank capacity | 2,207 l |
| Baggage volume | Add |
| Dimensions | |
| Seats | 2 |
| Seats - business class | Add |
| Seats - first class | Add |
| Cabin height | Add |
| Cabin width | Add |
| Cabin length | Add |
| Exterior length | 14.14 m |
| Tail height | 3.92 m |
| Fuselage diameter | 1 m |
| Wing span | 7.7 m |
| Wing tips | No Winglets |
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There was one edit, no edits waiting approval. Last edited by qjast(1747), Oct 26, 2021 (41 fields were changed)
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