000			00975nam a2200169Ia 4500
008			240126s9999 xx 000 0 und d
041			_aEnglish
082			_aPRME07-1135
100			_aHegde, Shashank G, Srinidhi S,Sudarshan P N
245		0	_aDesign And Development of Simplex Atomizer [Electronic Resource : Project Report] _bJagadeesh, Y J
260			_bPESIT, Dept. of ME, _aBangalore
440			_aNULL
520			_aFuel injectors form the main part of combustion system of an aircraft. The combustion system basically determines the power or thrust that the engine provides. The design of the combustion system is critical for the optimum performance of the engine. A jet engine whose thrust is in the range of 20 to 60 pounds is known as a micro-jet engine. Micro-jet engines find applications on such platforms like unmanned aerial vehicles, pilotless target aircraft etc.
650			_aMechanical
650			_aSimplex,Atomizer,Project,Report
942			_cPR
999			_c256691 _d256691