![wiring audio jack c230 kompressor 2004 wiring audio jack c230 kompressor 2004](https://d3d71ba2asa5oz.cloudfront.net/12032071/images/seap-apd127r_999__1.jpg)
The objective is to enhance the performance of an existing single-spool expendable turbojet engine in terms of. A theoretical study related to a short afterburner design is presented in this paper. bomber capable of maintaining speeds in excess of Mach 2.
![wiring audio jack c230 kompressor 2004 wiring audio jack c230 kompressor 2004](https://www.qxsmwihd.com/images-hd/HDRS0vQFyQB7PM01lvk9qxat/steeringpart/zxb-c230-64001/detail/zxb-c230-64001(27).jpg)
The engine was used on the Convair B-58 Hustler, the first U.S.
![wiring audio jack c230 kompressor 2004 wiring audio jack c230 kompressor 2004](https://dz310nzuyimx0.cloudfront.net/strapr1/9bcdf3949d096805472968d00323d4e8/28005b91dc1807469281dd4a328398a1.png)
The engine generated a maximum of 17,000 pounds of thrust (-15 version) with the afterburner operating. The development of the J79 turbojet began in 1952 as a more powerful follow-up to the General Electric J47 turbojet. The afterburner increases engine thrust by 59.6%. The maximum thrust with afterburning is 63.70 kN (6 495 kG). The maximum thrust without afterburning is 39.90 kN (4,068 kG).