Given: You will be analyzing the Lance Missile trajectory that is

launched in an inclined vertical trajectory. Using the data and simplifying assumptions

show below:

Find: $($a$)$ Burnout velocity of the Missile in $\frac{m}{s}$

$($b$)$ Launch angle of the missile in degrees from horizontal in degrees

$($c$)$ Apogee altitude in meters, if the missile were launched vertically

Assume:

a$)$ The vehicle is a point mass

b$)2-$D trajectory

c$)$ The initial velocity is vf at launch $(z=0)$

d$)$ No aerodynamic drag

e$)$ Velocity is zero at apogee

f$)$ Gravity is constant.

g$)$ Range is in the z$-$direction and altidute is in the y$-$direction