Answer:
r = 4.24x10⁴ km.
Explanation:
To find the radius of such an orbit we need to use Kepler's third law:
<em>where T₁: is the orbital period of the geosynchronous Earth satellite = 1 d, T₂: is the orbital period of the moon = 0.07481 y, r₁: is the radius of such an orbit and r₂: is the orbital radius of the moon = 3.84x10⁵ km. </em>
From equation (1), r₁ is:
Therefore, the radius of such an orbit is 4.24x10⁴ km.
I hope it helps you!
Answer:
K.E₂ = mg(h - 2R)
Explanation:
The diagram of the car at the top of the loop is given below. Considering the initial position of the car and the final position as the top of the loop. We apply law of conservation of energy:
K.E₁ + P.E₁ = K.E₂ + P.E₂
where,
K.E₁ = Initial Kinetic Energy = (1/2)mv² = (1/2)m(0 m/s)² = 0 (car initially at rest)
P.E₁ = Initial Potential Energy = mgh
K.E₂ = Final Kinetic Energy at the top of the loop = ?
P.E₂ = Final Potential Energy = mg(2R) (since, the height at top of loop is 2R)
Therefore,
0 + mgh = K.E₂ + mg(2R)
<u>K.E₂ = mg(h - 2R)</u>
Answer:
The fraction of the total initial kinetic energy is lost during the collision is
Explanation:
Given that,
Mass of one piece = 300 g
Speed of one piece = 1 m/s
Mass of other piece = 600 g
Speed of other piece = 0.75 m/s
We need to calculate the final velocity
Using conservation of energy
Put the value intro the formula
We need to calculate the total initial kinetic energy
Using formula of kinetic energy
Put the value into the formula
We need to calculate the total final kinetic energy
Using formula of kinetic energy
Put the value into the formula
We need to calculate the energy lost during the collision
Using formula of energy lost
Hence, The fraction of the total initial kinetic energy is lost during the collision is