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प्रश्न
A satellite of mass 'm' is revolving around the earth of mass 'M' in an orbit of radius 'r' with constant angular velocity 'ω'. The angular momentum of the satellite is ______.
(G =gravitational constant)
विकल्प
`((GMr)/m)^2`
`m(GMr)^(1/2)`
m(GMr)
`(GMmr)^(1/2)`
MCQ
रिक्त स्थान भरें
उत्तर
A satellite of mass 'm' is revolving around the earth of mass 'M' in an orbit of radius 'r' with constant angular velocity 'ω'. The angular momentum of the satellite is `underline(m(GMr)^(1/2))`.
Explanation:
Angular momentum `=mvr=msqrt((GM)/r)r`
`=msqrt(GMr)`
`=m(GMr)^(1/2)`
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