A first stage solid rocket has the following characteristics:Sea$-$Level Thrust is $200,512\mathrm{.}1/$bfMass flow rate is $799\mathrm{.}47$ Ibm$/$sNozzle Exit Pressure is $8\mathrm{.}70$ psiThroat area is $167\mathrm{.}1$ in$?$Area ratio is $10\mathrm{.}32$Find The Vacuum Thrust in Ibf