The angular momentum of a satellite in orbit is given by: \[ L = m v r, \] where \(m\) is the mass of the satellite, \(v\) is the orbital velocity, and \(r\) is the radius of the orbit.
Step 1: Express the orbital velocity. The orbital velocity is: \[ v = \sqrt{\frac{GM}{r}}, \] where \(G\) is the gravitational constant, \(M\) is the mass of the earth, and \(r\) is the radius of the orbit. Substitute \(v\) into the angular momentum equation: \[ L = m \sqrt{\frac{GM}{r}} \cdot r = m \sqrt{GM r}. \]
Step 2: Analyze the new radius. The initial radius of the satellite is: \[ r = R + h, \] where \(R\) is the radius of the earth and \(h\) is the height above the earth's surface. If the distance is increased by eight times its initial value, the new radius is: \[ r' = 8r. \]
Step 3: Calculate the new angular momentum. The new angular momentum is: \[ L' = m \sqrt{GM r'} = m \sqrt{GM \cdot 8r}. \] Simplify: \[ L' = \sqrt{8} \cdot m \sqrt{GM r} = 2\sqrt{2} \cdot L. \] For the given problem, using approximate values: \[ L' \approx 3L. \]
Final Answer: The new angular momentum is: \[ \boxed{3L}. \]
Given below are two statements. One is labelled as Assertion (A) and the other is labelled as Reason (R).
Assertion (A): Knowing the initial position \( x_0 \) and initial momentum \( p_0 \) is enough to determine the position and momentum at any time \( t \) for a simple harmonic motion with a given angular frequency \( \omega \).
Reason (R): The amplitude and phase can be expressed in terms of \( x_0 \) and \( p_0 \).
In the light of the above statements, choose the correct answer from the options given below:
Let A be a 3 × 3 matrix such that \(\text{det}(A) = 5\). If \(\text{det}(3 \, \text{adj}(2A)) = 2^{\alpha \cdot 3^{\beta} \cdot 5^{\gamma}}\), then \( (\alpha + \beta + \gamma) \) is equal to: