| Manufacturer | Lockheed |
| Model | TR-1 Dragon Lady |
| Modification | TR-1 |
| Country | USA |
| Years | 1979 |
| Type | Reconnaissance aircraft |
| Main rotor diameter | - |
| Tail rotor diameter | - |
| Wingspan | 31.39 m |
| Length | 19.13 m |
| Height | 4.88 m |
| Wing area | 92.90 m2 |
| Zero fuel weight | - |
| Empty weight | 4536 kg |
| Maximum takeoff weight | 18733 kg |
| Normal takeoff weight | 7031 kg |
| Flight duration | 12 h |
| Engine | 1 ТРД Pratt Whitney J75-P-13B |
| Power | - |
| Thrust | 1 x 75.62 kN |
| Maximum speed | - |
| Cruising speed | 692 km/h |
| Rate of climb | - |
| Practical range | 4828 km |
| Service ceiling | 27430 m |
| Hovering ceiling | - |
| Crew | 1 |
