An item designed to accelerate a gas turbine engine from rest to starter cutoff speed by means of a combustion gas driven turbine and reduction gear assembly constructed to be mounted on the engine starter drive. The combustion gas is generated from ignited liquid fuel and air in the combustion chamber or from a solid propellant cartridge attached to the combustion chamber of the starter. May have provision for energizing the turbine by low pressure air from engine bleed or ground equipment air supply.
Classification: Parts of gas turbine aircraft engines, other than for use in civil aircraft
NSN 5996-00-941-6200
NSN 5965-01-433-1974
NSN 6135-01-415-1163
NSN 6610-01-444-8881
NSN 5895-01-255-1690
NSN 6320-01-308-9392
NSN 5965-00-539-7778
NSN 6145-01-012-5008
NSN 5920-00-127-9992
NSN 5990-00-828-1771
NSN 5975-00-445-7264
NSN 5965-01-258-5662