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Answer :
The corresponding distance traveled by the orbiter is 224,761.8 miles
To calculate the distance traveled by the orbiter while the drag parachute is deployed, we need to first determine the time it takes for the speed to decrease from 221 mi/hr to 28 mi/hr.
We can use the formula:
t = (v2 - v1) / a
where t is the time, v2 is the initial speed, v1 is the final speed, and a is the deceleration.
Plugging in the given values, we find that t = 1,648 seconds.
The corresponding distance traveled by the orbiter can be calculated using the formula:
s = v2 * t + 0.5 * a * t2
Substituting the values, we find that s = 224,761.8 miles.
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