Answer:
Explanation:
Given
acceleration of rocket(a)[tex]=5 m/s^2[/tex]
At h=1000 m rocket burn out
[tex]v^2-u^2=2as[/tex]
[tex]v^2-0=2\times 5\times 1000[/tex]
[tex]v=\sqrt{10^4}=100 m/s[/tex]
(b) time to reach v=100 m/s
v=u+at
[tex]100=0+5\times t[/tex]
[tex]t=\frac{100}{5}=20 s[/tex]
(c)Rocket maximum altitude
[tex]v^2-u^2=2as[/tex]
here u=100 m/s
v=0
[tex]a=9.8 m/s^2[/tex]
[tex]s=\frac{v^2}{2g}[/tex]
[tex]s=\frac{100^2}{2\times 9.8}[/tex]
[tex]s=510.204
Therefore maximum altitude=510.204+1000=1510.204 m