Match the following for a satellite in circular orbit- Column-I - - Column-IIMWhinea- text Kinetic energy - p -d- e n d a r r a y -1A- a - s - b - r - c - p - d - q -B- a - r - b - s - c - q - d - p C- a - s - b - r - c - q - d - p D- a - r - b - s - c - q - d - p -

The correct option is A (a) → (s); (b) → (r); (c) → (p); (d) → (q);These are basic results that you can derive from conservation of energy. ...

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Byju's Answer

Standard XII

Physics

Gravitational Potential Energy of a Two Mass System

Match the fol...

Question

Match the following (for a satellite in circular orbit)
$\begin{matrix} C o l u m n - I & C o l u m n - I I (a) & Kinetic energy & (p) & - \frac{G M m}{2 r} (b) & Potential energy & (q) & \sqrt{\frac{G M}{r}} (c) & Total energy & (r) & - \frac{G M m}{r} (d) & Orbital velocity & (s) & \frac{G M m}{2 r} \end{matrix}$

(a)

\to

(s); (b)

\to

(r); (c)

\to

(p); (d)

\to

(q);

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(a)

\to

(r); (b)

\to

(s); (c)

\to

(q); (d)

\to

(p);

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(a)

\to

(s); (b)

\to

(r); (c)

\to

(q); (d)

\to

(p);

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(a)

\to

(r); (b)

\to

(s); (c)

\to

(q); (d)

\to

(p);

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Solution

The correct option is A (a) $\to$ (s); (b) $\to$ (r); (c) $\to$ (p); (d) $\to$ (q);
These are basic results that you can derive from conservation of energy.

Suggest Corrections

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Choose the correct option:

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and

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Match the following (for a satellite in circular orbit) Column−IColumn−II(a)Kinetic energy(p)−GMm2r(b)Potential energy(q)√GMr(c)Total energy(r)−GMmr(d)Orbital velocity(s)GMm2r

The correct option is A (a) → (s); (b) → (r); (c) → (p); (d) → (q);These are basic results that you can derive from conservation of energy.

The correct option is A (a) $\to$ (s); (b) $\to$ (r); (c) $\to$ (p); (d) $\to$ (q);
These are basic results that you can derive from conservation of energy.