A rocket vertically from
the surface of the earth
with an initil velocity(v_o )
show that its velocity v
at height h is given by
v_o ^2 −v^2 =((2gh)/(1+(h/R)))
where R is radius of earth
and g is the acceleration
due to gravity at the earth
surface
let f(x), g(x) and h(x) be functions
R→R, given by
f(x)=x^2 , if x≥0 and x+1 if x<0
g(x)=x^2 −4, if x≥2 and (1/(2−x)) if x<2
h(x)=3^(−x) , if x≤0 and 3^x if x≥0
Calculate ((f(2)+f(g(2)))/(f(g(h(−1))))).