General Electric J85 | Wikipedia audio article
Channel: wikipedia tts
Date: 2019-01-19

This is an audio version of the Wikipedia Article:
https://en.wikipedia.org/wiki/General_Electric_J85


00:01:03 1 Design and development
00:03:35 1.1 Iranian reverse engineering
00:04:01 2 Variants
00:07:22 3 Applications
00:08:36 3.1 Other
00:08:52 4 Specifications
00:09:03 4.1 General characteristics
00:09:45 4.2 Components
00:10:07 4.3 Performance
00:11:07 5 See also



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SUMMARY
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The General Electric J85 is a small single-shaft turbojet engine. Military versions produce up to 2,950 lbf (13.1 kN) of thrust dry, afterburning variants can reach up to 5,000 lbf (22 kN). The engine, depending upon additional equipment and specific model, weighs from 300 to 500 pounds (140 to 230 kg). It is one of GE's most successful and longest in service military jet engines, with the civilian versions having logged over 16.5 million hours of operation. The United States Air Force plans to continue using the J85 in aircraft through 2040. Civilian models, known as the CJ610, are similar but supplied without an afterburner, while the CF700 adds a rear-mounted fan for improved fuel economy.