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 5960-01-512-0233
NSN 5960-00-497-7657
NSN 5855-00-256-5562
NSN 5930-01-062-0734
NSN 6220-01-443-7731
NSN 6320-00-725-0754
NSN 5910-00-726-9114
NSN 6150-01-202-3237
NSN 5985-01-362-3921
NSN 6145-01-277-1173
NSN 6320-00-456-2092
NSN 5920-01-353-2487