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 5999-01-573-8371
NSN 5915-00-032-9734
NSN 5999-00-971-2361
NSN 5998-01-245-9124
NSN 5915-01-274-1411
NSN 5855-00-198-3197
NSN 6135-01-461-2915
NSN 6610-00-146-2269
NSN 5905-01-498-1079
NSN 5996-00-853-9067
NSN 5895-00-878-4617
NSN 5855-01-348-6690