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mestny [16]
3 years ago
7

Does energy or matter ever disappear? Explain.

Physics
2 answers:
Levart [38]3 years ago
8 0

Answer:

The law of Conservation of Energy states that "Energy cannot be created or destroyed.". In other words, the total amount of energy in the universe never changes, although it may change from one form to another. Energy never disappears, but it does change form.

Explanation:

maria [59]3 years ago
3 0

Answer:

The first law of thermodynamics doesn't actually specify that matter can neither be created nor destroyed, but instead that the total amount of energy in a closed system cannot be created nor destroyed (though it can be changed from one form to another).

Explanation:

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3 years ago
If a net force of 34.3 N is required to move the system in the figure to the right 2.3 m in 1.3 seconds what is the systems mass
sasho [114]
Mass of the system is 25.2 kg
Calculation:

F=ma

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a=2.3/(1.3)^2 = 1.36 m/s^2

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3 years ago
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S_A_V [24]

Answer:

13.4s

Explanation:

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8 0
2 years ago
Io and Europa are two of Jupiter's many moons. The mean distance of Europa from Jupiter is about twice as far as that for Io and
Anastaziya [24]

The universal gravitation law and Newton's second law allow us to find that the answer for the relation of the rotation periods of the satellites is:

        \frac{T_{Eu}}{T_{Io}} = 2.83

The universal gravitation law states that the force between two bodies is proportional to their masses and inversely proportional to their distance squared

           F = G  \frac{Mm}{r^2}

Where G is the universal gravitational constant (G = 6.67 10⁻¹¹ \frac{N m^2 }{kg^2}), F the force, m and m the masses of the bodies and r the distance between them

Newton's second law states that force is proportional to the mass and acceleration of bodies

          F = m a

Where F is the force, m the mass and the acceleration

In this case the body is the satellites of Jupiter and the planet,

            G \frac{Mm}{r^2} = m a

Suppose the motion of the satellites is circular, then the acceleration is centripetal

           a = \frac{v^2}{r}r

Where v is the speed of the satellite and r the distance to the center of the planet

     

we substitute

      G \frac{Mm}{r^2} = m \frac{v^2}{r}  \\G \frac{M}{r}  = v^2

Since the speed is constant, we can use the uniform motion ratio

      v = \frac{\Delta x}{t}

In the case of a complete orbit, the time is called the period.

The distance traveled is the length of the orbit circle

           Δx = 2π r

We substitute

           G \frac{M}{r} = (\frac{2 \pi  r}{T} )^2 \\T^2 = (\frac{4 \pi ^2}{GM}) \ r^3

           

Let's write this expression for each satellite

Io satellite

Let's call the distance from Jupiter is  

            r = r_{Io}  

           T_{Io}^2 = (\frac{4 \pi ^2}{GM} ) \ r_{Io}^3TIo² = (4pi² / GM) rIo³

Europe satellite

Distance from Jupiter  is

         r_{Eu} = 2 \ r_{Io}

We calculate

         T_{Eu} = ( \frac{4\pi ^2 }{GM} (2 \ r_{Io})^3\\T_{Eu} = ( \frac{4 \pi ^2 }{GM}) r_{Io} \ 8

         

         T_{Eu}^2 = 8 T_{Io}^2            

         

         \frac{ T_{Eu}}{T_{Io}} = \sqrt{8}  = 2.83

           

In conclusion, using the universal gravitation law and Newton's second law, we find that the answer for the relationship of the relation periods of the satellites is:

        \frac{T_{Eu}}{T_{Io}} = 2.83

Learn more about universal gravitation law and Newton's second law here:

brainly.com/question/10693965

6 0
2 years ago
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