| Parade Ground Aircraft | |||||||||||
| A7 | A10 | B17 | B24 | B25 | B26 | B29 | C45 | C47 | C118 | C119 | C121 |
| C123 | F15 | F16 | F82 | P38 | P47 | P51 | P63 | SR71 | T6 | T28 | T34 |
| Other USAF Aircraft | |||||||||||
| Bombers | |||||||||||
| B1 | B2 | B45 | B47 | B50 | B52 | B58 | F111 | - | - | - | - |
| Cargo, VIP, & Tanker | |||||||||||
| C5 | C17 | C21 | C24 | C46 | C97 | C130 | C133 | C140 | C141 | KC10 | KC135 |
| Experimental & Prototype | |||||||||||
| D558 | F107 | X1 | X2 | X3 | X4 | X5 | X15 | XB70 | YC14 | - | - |
| Fighters | |||||||||||
| A1 | F4 | F5 | F22 | F84 | F84F | F86 | F86D | F100 | F101 | F102 | F104 |
| F105 | F106 | F117 | P40 | P80 | - | - | - | - | - | - | - |
| Helicopters | |||||||||||
| CH3E | CH21 | CH54A | H5A | HH43 | MH60 | R4B | R6A | UH1P | UH13 | UH19 | V22 |
| Reconnaissance | |||||||||||
| E3 | O1G | OV2 | OV10 | RF4 | RF101 | U2 | - | - | - | - | - |
| Trainers | |||||||||||
| T6A | T33 | T37 | T38 | T41 | - | - | - | - | - | - | - |
Lockheed U-2 Spy Plane

The U-2 provides continuous day or night, high-altitude, all-weather, stand-off surveillance of an area in direct support of U.S. and allied ground and air forces. It provides critical intelligence to decision makers through all phases of conflict, including peacetime indications and warnings, crises, low-intensity conflict and large-scale hostilities. When requested, the U-2 also has provided photographs to the Federal Emergency Management Agency in support of disaster relief. The U-2 is a single-seat, single-engine, high-altitude, reconnaissance aircraft. Long, wide, straight wings give the U-2 glider-like characteristics. It can carry a variety of sensors and cameras, is an extremely reliable reconnaissance aircraft, and enjoys a high mission completion rate. However, the aircraft can be a difficult aircraft to fly due to its unusual landing characteristics. Because of its high altitude mission, the pilot must wear a full pressure suit.
Primary Function: high-altitude reconnaissance
Contractor: Lockheed Aircraft Corp. VARIANT U-2A U-2R TR-1 U-2S
Wing span: 80 feet 103 feet
Length: 49.5 feet 63 feet
Empty Weight: 11,700 lbs 14,900 lbs 16,000 lbs
Maximum Takeoff Weight: 16,000 lb 41,000 lb (18,598 kg)
Maximum Speed: 528 mph 510 mph 495 mph ~500 mph
Engine: P&W J57-P-37A P&W J75-P-13B GE F-118-101
Engine Thrust: 11,200 lbst 17,000 lbst 19,000 lbst
Ceiling: 85,000 feet 80,000 feet 90,000 feet
Range: 2,200 miles 3,500 miles 4,000 miles 4,600 miles
Endurance: on internal fuel 6.5 hours 7.5 hours 12 hours +10 hours
Date Deployed: Aug 1955, 1967, Sep 1981, Oct 1994
Crew: One (two in trainer models)
Cost: Classified $400 million







![]() |
| Parade Ground Aircraft | |||||||||||
| A7 | A10 | B17 | B24 | B25 | B26 | B29 | C45 | C47 | C118 | C119 | C121 |
| C123 | F15 | F16 | F82 | P38 | P47 | P51 | P63 | SR71 | T6 | T28 | T34 |
| Other USAF Aircraft | |||||||||||
| Bombers | |||||||||||
| B1 | B2 | B45 | B47 | B50 | B52 | B58 | F111 | - | - | - | - |
| Cargo, VIP, & Tanker | |||||||||||
| C5 | C17 | C21 | C24 | C46 | C97 | C130 | C133 | C140 | C141 | KC10 | KC135 |
| Experimental & Prototype | |||||||||||
| D558 | F107 | X1 | X2 | X3 | X4 | X5 | X15 | XB70 | YC14 | - | - |
| Fighters | |||||||||||
| A1 | F4 | F5 | F22 | F84 | F84F | F86 | F86D | F100 | F101 | F102 | F104 |
| F105 | F106 | F117 | P40 | P80 | - | - | - | - | - | - | - |
| Helicopters | |||||||||||
| CH3E | CH21 | CH54A | H5A | HH43 | MH60 | R4B | R6A | UH1P | UH13 | UH19 | V22 |
| Reconnaissance | |||||||||||
| E3 | O1G | OV2 | OV10 | RF4 | RF101 | U2 | - | - | - | - | - |
| Trainers | |||||||||||
| T6A | T33 | T37 | T38 | T41 | - | - | - | - | - | - | - |