Part Details | TURBO-JET ENGINE
2840-01-286-9609 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: J402CA702, J402-CA-702, 13284108, 2840-01-286-9609, 01-286-9609, 2840012869609, 012869609
| Supply Group (FSG) | NSN Assigned | NIIN | Item Name Code (INC) |
|---|---|---|---|
| 28 | OCT 12, 1988 | 01-286-9609 | 02007 ( ENGINE, TURBO-JET ) |
REFERENCE DRAWINGS & PICTURES
Cross Reference | NSN 2840-01-286-9609
| Part Number | Cage Code | Manufacturer |
|---|---|---|
| J402-CA-702 | 03104 | TELEDYNE TECHNOLOGIES INCORPORATEDDBA TELEDYNE TURBINE ENGINES |
| 13284108 | 18876 | U S ARMY AVIATION AND MISSILECOMMAND |
Technical Data | NSN 2840-01-286-9609
| Characteristic | Specifications |
|---|---|
| END ITEM IDENTIFICATION | TARGETS, SURFACE TO AIR MISSILES |