Respuesta :
Answer:
the ship's energy is greater than this and the crew member does not meet the requirement
Explanation:
In this exercise to calculate kinetic energy or final ship speed in the supply hangar let's use the relationship
W =∫ F dx = ΔK
Let's replace
∫ (α x³ + β) dx = ΔK
α x⁴ / 4 + β x = ΔK
Let's look for the maximum distance for which the variation of the energy percent is 10¹⁰ J
x (α x³ + β) = [tex]K_{f}[/tex] - K₀
[tex]K_{f}[/tex] = K₀ + x (α x³ + β)
Assuming that the low limit is x = 0, measured from the cargo hangar
Let's calculate
[tex]K_{f}[/tex] = 2.7 10¹¹ + 7.5 10⁴ (6.1 10⁻⁹ (7.5 10⁴) 3 -4.1 10⁶)
Kf = 2.7 10¹¹ + 7.5 10⁴ (2.57 10⁶ - 4.1 10⁶)
Kf = 2.7 10¹¹ - 1.1475 10¹¹
Kf = 1.55 10¹¹ J
In the problem it indicates that the maximum energy must be 10¹⁰ J, so the ship's energy is greater than this and the crew member does not meet the requirement
We evaluate the kinetic energy if the System is well calibrated
W = x F₀ = [tex]K_{f}[/tex] –K₀
[tex]K_{f}[/tex] = K₀ + x F₀
We calculate
[tex]K_{f}[/tex] = 2.7 10¹¹ -7.5 10⁴ 3.5 10⁶
[tex]K_{f}[/tex] = (2.7 -2.625) 10¹¹
[tex]K_{f}[/tex] = 7.5 10⁹ J
The value of final kinetic energy of the spacecraft is [tex]1.075 \times 10^{10} \;\rm J[/tex].
Given data:
The value of F is, [tex]F(x)= \alpha x^{3}+\beta[/tex].
The constant beam force is, [tex]F_{0}=-3.5 \times 10^{6} \;\rm N[/tex].
The value of constants are, [tex]\alpha = 6.1 \times 10^{-9} \;\rm N \;\;\;\rm and \;\;\;\;\rm \beta = -4.1 \times 10^{6}\;\rm N[/tex].
The initial kinetic energy is, [tex]KE_{1}=2.7 \times 10^{11} \;\rm J[/tex].
And distance is, [tex]x = 7.5 \times 10^{4} \;\rm m[/tex]
In the given problem, it is required to obtain the value of final kinetic energy. For this, use the relation of work- energy as,
[tex]W= \int {F} \, dx= \Delta KE[/tex]
here, F is the force exerted by the tractor beam and dx is the position function.
Solving as,
[tex]\int {(\alpha x^{3}+\beta)} \, dx=\Delta KE\\\\\dfrac{\alpha x^{4}}{4}+ \beta x=\Delta KE[/tex]
Let's look for the maximum distance for which the variation of the energy percent is [tex]10^{10} \;\rm J[/tex].
[tex]\dfrac{\alpha x^{4}}{4}+ \beta x= KE_{2}-KE_{1}\\\\\dfrac{6.1 \times 10^{-9} \times (7.5 \times 10^{4})^{4}}{4}+ (-4.1 \times 10^{6} \times 7.5 \times 10^{4})= KE_{2}-(2.7 \times 10^{11})\\\\KE_{2} = 1.075 \times 10^{10} \;\rm J[/tex]
Thus, we can conclude that the value of final kinetic energy of the spacecraft is [tex]1.075 \times 10^{10} \;\rm J[/tex].
Learn more abut the work-energy theorem here:
https://brainly.com/question/24509770