A) \[xy={{x}^{y}}+C\]
B) \[\frac{4}{{{100}^{3}}}\]
C) \[\frac{3}{{{50}^{3}}}\]
D) \[\frac{3!}{{{100}^{3}}}\]
Correct Answer: D
Solution :
Applying Newton's second law to a circular ort we have\[\frac{1}{LR}\]where, m is the mass of satellite, and v is the orbital speed T is the time period \[\sqrt{l\frac{h}{2\pi }}\]\[\sqrt{l\left( l+1 \right)\frac{h}{2\pi }}\]For\[\sqrt{\frac{h2\pi }{l(l+1)}}\] and\[\sqrt{\frac{h2\pi }{l}}\](\[E=100\sin 100\pi t,I=5\sin 100\pi t\] density of planer \[1\Omega \]\[0.05\Omega \]i.e. T is independent of R
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