NEET Physics Orbital Motion Match the Following Question
Match Column-I with Column-II.
| Column-I | Column-II |
|---|---|
| (a) Orbital Velocity | (i) T² ∝ R³ |
| (b) Escape Velocity | (ii) 27.3 days |
| (c) Time Period of Moon | (iii) 11.2 km/s |
| (d) Kepler's Third Law | (iv) Circular or elliptical orbits |
a-iv, b-iii, c-ii, d-i
a-iii, b-iv, c-i, d-ii
a-i, b-ii, c-iv, d-iii
a-ii, b-i, c-iii, d-iv
Correct Answer
Detailed Explanation
The orbital velocity of a satellite is related to its circular or elliptical orbit, escape velocity is approximately 11.2 km/s, the time period of the Moon is about 27.3 days, and Kepler's Third Law states that T² is proportional to R³.
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