A model rocket blasts off from the ground, rising straight upward with a constant acceleration that has a magnitude of 74.3 m/s2 for 1.80 seconds, at which point its fuel abruptly runs out. Air resistance has no effect on its flight. What maximum altitude (above the ground) will the rocket reach?
Given:
"v_0=0, \\; a=74.3\\:{\\rm m\/s},\\; t=1.80\\:\\rm s"
Hence, the maximum altitude that the rocket will reach
"h=at^2\/2+\\frac{(at)^2}{2g}""h=74.3*1.80^2\/2+(74.3*1.80)^2\/(2*9.81)\\\\\n=1032\\:\\rm m"
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