seconds after liftoff. $($Give the upper approximation available from the data.$)$

$h=q,$ ft

$\backslash$table$[[$Event$,$Time $($s$),$Velocity $($ft$/$s$)],[$Launch$,0,0],[$Begin roll maneuver,$10,180],[$End roll maneuver,$15,319],[$Throttle to $89\%,20,442],[$Throttle to $67\%,32,742],[$Throttle to $104\%,59,1217],[$Maximum dynamic pressure,$62,1453],[$Solid rocket booster separation,$125,4151]]$