The J75 was a scaled up J57 and first flew in 1955. This turbojet was in production from 1956 through 1967.

models

• YJ75-P-11: 23,500 lb (104.5 kN) afterburning thrust
• J75-P-17: 24,500 lb (109 kN) afterburning thrust
• J75-P-19W: 24,500 lb (109 kN) afterburning thrust

specifications

• Turbojet
• Dual compressor, axial flow
• mass flow: 249-256 lbs/sec

used by

• Republic F-105 Thunderchief
• Convair F-106 Delta Dart
• North American F-107
• Martin P6M Seamaster