small engines apus design and development archived 10 2006 bet shemesh sorek iv the israel is a single shaft axial centrifugal flow expendable turbojet engine maximum rated 809 lbst 3 6 kn well suited for target applications subsonic cruise missiles rpvs in same general class as teledyne j402 williams international f107 microturbo tri 60 it was reported 1982 that this production at while initial ivs are unaugmented we believe can be configured with an afterburner extra zero stage compressor fan module to increase thrust specific of israeli built have not been officially divulged most current application aircraft industries iai gabriel mk missile also referred long range glr air breathing designed pene tration naval defense systems were anticipated 1990s 1992 halted further having purchased agm 84 harpoon mission requirement taiwan
