Part Details | TURBO-JET ENGINE
2840-01-135-2555 A continuous-combustion type power unit, may be with or without container, designed to exert thrust. It's prime physical characteristics include air compressor(s), combustion chamber(s) and gas turbine. The operating principle is as follows: atmospheric air is inducted into the unit at its front, compressed, heated by combustion of a fuel, expanded through the gas turbine, and ejected at high velocity. It may incorporate features to vary direction of the thrust.
Alternate Parts: 642AS02372, 642AS0237-2, 642AS02371, 642AS0237-1, 642AS0237, 642AS02372, 642AS0237-2, 2840-01-135-2555, 01-135-2555, 2840011352555, 011352555
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | JUL 20, 1982 | 01-135-2555 | 02007 ( ENGINE, TURBO-JET ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-135-2555
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| 642AS0237-2 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
| 642AS0237-1 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
| 642AS0237 | 30003 | NAVAL AIR SYSTEMS COMMAND MANAGEDORIGINAL DESIGN ACTIVITY NOT |
| 642AS0237-2 | 03104 | TELEDYNE TECHNOLOGIES INCORPORATEDDBA TELEDYNE TURBINE ENGINES |
Technical Data | NSN 2840-01-135-2555
| Characteristic | Specifications |
|---|---|
| SPECIAL FEATURES | GENERAL CHARACTERISTICS ITEM DESCRIPTION:ITEM CONSISTS OF TURBOJET ENGINE J402-CA-400 PLUS INSTALLATION COMPONENTS, HAS A NEW OR REWORKED FUEL CONTROL ELECTRONICS UNIT P/N 722070-3 AND 722825 OR 722068 AND 722070 |