The U-2A is powered by a 10,500-pound thrust J57-P-37A engine produced by Pratt & Whitney. In 1958, the U-2A replaced the J75-P-13A engine with a thrust of 15,800 pounds and was upgraded to the U-2C. In 1959, in order to increase the air intake of the U-2C engine, the intake port was modified and enlarged. In 1966, the U-2C was replaced with a 17,000-pound thrust J75-P-13B engine, and the air intake was modified again. In 1967, the redesigned U-2R with more endurance and more payload began to fly. By 1968, the U-2R had replaced the heavily depleted U-2C, and another series of U-2 fleets had entered service.
- Landing-gear doors can be selected position in open or closed.
- Airbrake can be selected position in open or closed.
- Accurate cockpit details.
- Appropriative"type b" camera only for u-2c.
- "Type b" camera can be displayed independently.
- Two types intake.
- Long dorsal electronics fairing.
- "Sugar scoop" infrared deflector.
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