Mgeneral 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
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.
Classification: Turbojet aircraft turbines (engines) other than for civil aircraft, of a thrust not exceeding 25 kn
NSN 5925-00-852-7809
NSN 5945-00-966-4567
NSN 6130-01-543-5798
NSN 5960-01-502-6270
NSN 5835-00-898-0201
NSN 2925-01-025-0082
NSN 6620-00-485-4136
NSN 6135-01-433-2062
NSN 7035-01-382-4413
NSN 5910-01-444-1429
NSN 5925-00-064-9873
NSN 5930-00-730-9214