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irakobra [83]
3 years ago
7

An asteroid, whose mass is 4.20×10⁻⁴ times the mass of Earth, revolves in a circular orbit around the Sun at a distance that is

6 times the Earth's distance from the Sun. Calculate the period of revolution of the asteroid.
Physics
1 answer:
vlabodo [156]3 years ago
3 0

Answer:

The time period of revolution of the asteroid is 14.69 years.

Explanation:

Given that,

Mass of asteroid M= 4.20\times10^{-4}M_{e}

Distance r= 6r_{e}

We need to calculate the velocity

Using relation centripetal force and gravitational force

\dfrac{mv^2}{r}=\dfrac{GMm}{r^2}

v^2=\sqrt{\dfrac{GM}{r}}

We need to calculate the time period of revolution of the asteroid

Using formula of time period

T=\dfrac{2\pi r}{v}

Put the value of v into the formula

T=\dfrac{2\pi r}{\sqrt{\dfrac{GM}{r}}}...(I)

We need to calculate the time period of revolution of the earth

Using formula of time period

T_{e}=\dfrac{2\pi r}{v}

T_{e}=\dfrac{2\pi r_{e}}{\sqrt{\dfrac{GM_{e}}{r_{e}}}}....(II)

From equation (I) and (II)

\dfrac{T^2}{T_{e}^2}=(\dfrac{r}{r_{3}})^3

\dfrac{T^2}{T_{e}^2}=216

\dfrac{T}{T_{e}}=\sqrt{216}

\dfrac{T}{T_{e}}=14.69

T=14.69T_{e}

Hence, The time period of revolution of the asteroid is 14.69 years.

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Answer:

The resultant velocity of the helicopter is \vec v_{H} = \left(89.894\,\frac{m}{s}, -93.348\,\frac{m}{s}\right).

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Physically speaking, the resulting velocity of the helicopter (\vec v_{H}), measured in meters per second, is equal to the absolute velocity of the wind (\vec v_{W}), measured in meters per second, plus the velocity of the helicopter relative to wind (\vec v_{H/W}), also call velocity at still air, measured in meters per second. That is:

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In addition, vectors in rectangular form are defined by the following expression:

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\vec v_{H} = \left(\|\vec v_{W}\|\cdot \cos \alpha_{W}+\|\vec v_{H/W}\|\cdot \cos \alpha_{H/W}, \|\vec v_{W}\|\cdot \sin \alpha_{W}+\|\vec v_{H/W}\|\cdot \sin \alpha_{H/W} \right)

If we know that \|\vec v_{W}\| = 25\,\frac{m}{s}, \|\vec v_{H/W}\| = 125\,\frac{m}{s}, \alpha_{W} = 240^{\circ} and \alpha_{H/W} = 325^{\circ}, then the resulting velocity of the helicopter is:

\vec v_{H} = \left(\left(25\,\frac{m}{s} \right)\cdot \cos 240^{\circ}+\left(125\,\frac{m}{s} \right)\cdot \cos 325^{\circ}, \left(25\,\frac{m}{s} \right)\cdot \sin 240^{\circ}+\left(125\,\frac{m}{s} \right)\cdot \sin 325^{\circ}\right)\vec v_{H} = \left(89.894\,\frac{m}{s}, -93.348\,\frac{m}{s}\right)

The resultant velocity of the helicopter is \vec v_{H} = \left(89.894\,\frac{m}{s}, -93.348\,\frac{m}{s}\right).

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