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There is a page named "General Electric YJ101" on Wikipedia
The General Electric YJ101 was an afterburning turbojet engine, as signified by its "J" designation, in the 15,000 lbf class. It was designed for the Northrop...5 KB (454 words) - 14:11, 14 July 2023
(dry), 7.75 (afterburning) Related development General Electric YJ101 General Electric F414 General Electric F110 Volvo RM12 Comparable engines GTRE GTX-35VS...10 KB (1,132 words) - 04:10, 12 June 2024
engines. The aircraft was powered by two 14,400-pound-force (64 kN) General Electric YJ101-GE-100 afterburning turbojets, installed next to each other to minimize...16 KB (1,673 words) - 03:43, 9 May 2024
Volvo RM12 (section General characteristics)Thrust-to-weight ratio: 7.8 Related development General Electric YJ101 General Electric F404 General Electric F414 General Electric F110 Comparable engines GTRE GTX-35VS...10 KB (1,091 words) - 18:46, 1 June 2024- 1964, Woll led development of the 14,300 lbf (64 kN) thrust GE15 (later YJ101) which evolved into the F404 used in the McDonnell Douglas F/A-18 Hornet...4 KB (339 words) - 19:50, 4 May 2024
