The 236000-lb space-shuttle orbiter touches down at about 226 mi/hr. the drag chute is deployed at 207 mi/hr, the wheel brakes are applied at 99 mi/hr until wheelstop, and the drag chute is jettisoned at 39 mi/hr. if the drag chute results in a deceleration of -0.00043v2 (in feet per second squared when the speed v is in feet per second) and the wheel brakes cause a constant deceleration of 3.8 ft/sec2, determine the distance s traveled from 207 mi/hr to wheelstop