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| Lockheed Martin TR-1 |
| Origin: |
USA |
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| Type: |
single-seat high-altitude reconnaissance aircraft |
| Max Speed: |
692 km/h / 430 mph |
| Max Range: |
10050 km / 6,250 miles |
| Dimensions: |
span 31.39 m (103 ft 0 in)
length 19.13 m (62 ft 9 in)
height 4.88 m (16 ft 0 in) |
| Weight: |
empty 7031 kg (15,500 Ib); maximum take-off 18733 kg (41,300 Ib) |
| Powerplant: |
one 7711-kg (17,000-lb) dry thrust Pratt & Whitney J75-P-13B turbojet
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| Armament: |
none |
| Operators: |
United States (U-2 / TR-1) |
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