An artificial satellite is revolving around a planet of radius R in a circular orbit of radius ' a '. If the time period of revolution of the satellite, T \propto a^{3 \/ 2} g^x R^y, then the values of x and y are respectively [g - acceleration due to gravity] [AP EAPCET 23 May 2025 S2]

AP EAPCET 23 May 2025 Shift 2 Paper

Section: Physics

Question : 93 of 160

Marks: +1, -0

An artificial satellite is revolving around a planet of radius R in a circular orbit of radius ' a '. If the time period of revolution of the satellite, T∝a3∕2gxRy, then the values of x and y are respectively
[g - acceleration due to gravity]

[AP EAPCET 23 May 2025 S2]

‌‌1,
1
2
‌‌
1
2
,1
‌−‌
1
2
,‌
1
2
‌‌
−1
2
,−1

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