Pratt & Whitney J75 (JT4)

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The Engine

Specifications

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

Models

Used by

	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

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page updated 04 July 2003