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GIVEN THAT TET PROPELLED ARUNER fLIES AT ALTIDTUE OF 15,000mSO FIRST FIND THE STATIC PRESSURE & TEMPERATURE AT THIS ALTITUDET_(STATC)=216.862KquadP_("STATIC ")=12153.91paSO, WE KNOW THAT, ASSUMING ISENTROPIC PROCESS{:[(P_(t))/(p)=((T_(t))/(T))^((gamma)/(gamma-1))longrightarrow" (1) "],[" TSTAgrition "=T_("STATIC ")+(v^(2))/(2CP)],[:.T_(t)=216.802+(265^(2))/(2xx1005)],[T_(t)=216.862+34.9378=251.8K],[:.quad(P_(t))/(12153.91)=((251.8)/(216.862))^((1.4)/(0.4))],[P_(t)=1.6867 xx12153.91=2.05 xx10^(4)pa". "]:}From (1){:[(P_(E))/(p)=((Tt)/(T))^(gamma//gamma-1)=(1+(gamma-1)/(2)M^(2))^((gamma)/(gamma-1))],[(2.05 xx10^(4))/(12153.91)=(1+(1.4-1.m^(2))/(2))^((1.4)/(0.4))],[1.6867=(1+0.2m^(2))^(3.5)],[" M "=0.897*(" MACH NUMBER) "],[" kNOW THAT "]:}WE KNOW THAT-(gamma+1)/(2(gamma-1))m^(˙)=A(P_(t))/(sqrt(T_(t)))xxsqrt((gamma )/(R))M(1+(gamma-1)/(2)m^(2))1.AT GROUND LOCATON{:[m^(˙)=A xx(101325)/(sqrt298)xxsqrt((1.4)/(287))xx0.897(1+(1.41)/(2)xx0.897^(2))^(-(2.4)/(2xx0.4))],[=>40=A xx367.725 xx(1.1611)^(-3)],[A=0.17027]:}SINCE MACH NUMBER is SAME ABOVE AS WELL{:[m^(˙)=0.17027 xx(12153.91)/(sqrt(216*862))xxsqrt((1.4)/(287))xx0.897 xx(1.1611)^(-3)],[=5.58kgs]:} ...