Two small satellites move in circular orbits around the earth,at distance r and r+delta r from the centre of earth their time periods of rotation T and T+deltaT [delta r <<
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- Two small satellites move in circular orbits around the earth,at distance r and r+delta r from the centre of earth their time periods of rotation T and T+deltaT [delta r <<
Correct question may be ,
- Two small satellites move in circular orbits around the earth,at distance r and r+∆ r from the centre of earth their time periods of rotation T and T+∆T [delta r <<< r and ∆T <<< T ]
Here if you want the the derivation for ∆T
Then ,
Your Answer is ,
Given in the question ,
- Two satellites circulating in their orbits around the earth.
- The given distances from the centre of the earth to the orbits are r and r+∆r.
- Time periods of rotation for given satellites are T and T + ∆T.
Here , we can find the ∆T 's value
As we can say that , T ² directly proportional to the r³
So,
- T² = cr³ .............( 1 )
- we can express c as a constant.
Also from the question , we can say that ,
For the second satellite
- ( T + ∆T )² = c ( r + ∆ r )³
if r >>> ∆r and T >>> ∆T
Then ,
- T² + 2T∆T = c ( r³ + 3r²∆r )
in this equation we neglected ∆T² and ∆r³as r >>>∆r and T >>> ∆T ( Already discussed ).
- T² + 2T∆T = cr³ + c3r²∆r
By , putting the value of equation ( 1 ) in this equation , we get ,
- cr³ + 2T∆T = cr³ + c3r²∆r
- 2T∆T = c3r²∆r. ( new )
This new equation , when devided by equation ( 1 ) , we get ,
- 2T∆T / T² = c3r²∆r / cr³
- 2∆T / T = 3∆r / r
So ,
- ∆T = 3T∆r / 2r
→ We also can find the derivation for r and T now from same method
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