Consider a jet-powered combat aircraft with the following characteristics:
1. cruise Mach number $=2.1$;
2. max. Mach number $=1.9$;
3. cruise alt. $=60,000 \mathrm{ft}$;
4. oper. rad. $=300 \mathrm{~nm}$;
5. engine $\operatorname{TSFC}(\min / \max )=0.8 / 1.8$;
6. thrust $=22,000 \mathrm{lbs}$;
7. aspect ratio $=2.4$;
8. combat time $=8 \mathrm{~min}$;
9. combat alt. $=20,000 \mathrm{ft}$;
10. loiter time $=20 \mathrm{~min}$;
11. loiter altitude $=10,000 \mathrm{ft}$;
12. structure factor $=0.5$;
13. exp. payload $=0 \mathrm{lbs}$;
14. nonexp. payload $=600 \mathrm{lbs}$.
Determine the final take-off weight. How is this changed if the expendable payload is $500 \mathrm{lbs} ?$