Question #72235

An experiment rocket designed to land upright falls freely from a height of 2 x 10^2m, starting at rest. At a height of 80 m, the rocket's engines start. And provide constant upward acceleration until the rocket lands. What acceleration is required if the speed on touchdown is to be zero?
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Expert's answer

2018-01-04T04:38:41-0500

Answer on Question 72235 - Physics / Mechanics | Relativity

Question

An experiment rocket designed to land upright falls freely from a height of 2×102m2 \times 10^{\wedge}2\mathrm{m} , starting at rest. At a height of 80m80\mathrm{m} , the rocket's engines start. And provide constant upward acceleration until the rocket lands. What acceleration is required if the speed on touchdown is to be zero?

Solution. Draw the diagram for this task. Initial height of the rocket is y0=200my_0 = 200 \, \text{m} . Height



when the rocket's engines start is y1=80my_{1} = 80 \, \text{m} . Height of landing is y2=0y_{2} = 0 .

First we find the speed of the rocket just before the engines start, that is, for y=y1y = y_{1} . For this we use the formula for v2v^{2} at constant acceleration


v12=v02+2g(y0y1)v _ {1} ^ {2} = v _ {0} ^ {2} + 2 g \left(y _ {0} - y _ {1}\right)


where v0v_{0} is the initial speed of the rocket, v1v_{1} is the speed of the rocket at y=y1y = y_{1} , g=9.80m/c2g = 9.80\mathrm{m / c^2} is the acceleration due to gravity, (y0y1)(y_0 - y_1) is the distance that the rocket fell freely before the engines start. Since a rocket start at rest then v0=0v_{0} = 0 and we get


v12=2g(y0y1)v _ {1} ^ {2} = 2 g \left(y _ {0} - y _ {1}\right)


Now we find the required acceleration aa and use the same formula changing the subscripts


v22=v12+2a(y1y2)v _ {2} ^ {2} = v _ {1} ^ {2} + 2 a \left(y _ {1} - y _ {2}\right)


Here v1v_{1} is the initial speed before deceleration, v2=0v_{2} = 0 is the speed on touchdown, (y1y2)(y_{1} - y_{2}) is the distance that the rocket fell with deceleration. We get


a=v122(y1y2)a = - \frac {v _ {1} ^ {2}}{2 (y _ {1} - y _ {2})}


Substitution v12=2g(y0y1)v_{1}^{2} = 2g(y_{0} - y_{1}) yields


a=2g(y0y1)2(y1y2)=g(y0y1)(y1y2)a = - \frac {2 g (y _ {0} - y _ {1})}{2 (y _ {1} - y _ {2})} = - g \frac {(y _ {0} - y _ {1})}{(y _ {1} - y _ {2})}


Plugging y0=200my_0 = 200 \, \text{m} , y1=80my_1 = 80 \, \text{m} , y2=0y_2 = 0 and g=9.80m/c2g = 9.80 \, \text{m/c}^2 we get


a=9.8020080800=9.801.5=14.7m/c2a = - 9. 8 0 \frac {2 0 0 - 8 0}{8 0 - 0} = - 9. 8 0 \cdot 1. 5 = - 1 4. 7 \mathrm {m / c ^ {2}}


The minus sign of acceleration shows that the rocket is moving with deceleration

Answer: required acceleration is a=14.7m/c2a = -14.7 \, \text{m/c}^2 .

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