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CBSE Class 12-science Answered

Sir, how should we apply the energy conservation in case of taking a satellite to a height or moving a satellite from one orbit to another ?
Asked by minipkda | 22 May, 2018, 06:31: PM
answered-by-expert Expert Answer
When a satellite is orbiting in an orbit which is at a distance r from centre of earth(or any planet), we have potenial energy U that is given by
 
begin mathsize 12px style U space equals space minus G fraction numerator M space m over denominator r end fraction...................... left parenthesis 1 right parenthesis end style
Kinetic energy K begin mathsize 12px style equals space 1 half m v squared space equals space 1 half m space omega squared r squared space................. left parenthesis 2 right parenthesis end style
where v is the tangential speed and ω is angular speed of satellite in orbit.
 
we know that Gravitational force balance the centripetal force.
 
hence begin mathsize 12px style G fraction numerator M space m over denominator r squared end fraction space equals space fraction numerator m space v squared over denominator r end fraction space equals space m space omega squared space r end style...........................(3)
from eqn.(3), after simplification, we get begin mathsize 12px style omega squared space r squared space equals space G fraction numerator M m over denominator r end fraction end style ......................(4)
By substituting for ω2r2 using eqn.(4) in eqn.(2), we get kinetic energy K = begin mathsize 12px style G fraction numerator M space m over denominator 2 space r end fraction end style.................... (5)
Total energy U+K = begin mathsize 12px style equals space minus G fraction numerator M space m over denominator 2 space r end fraction end style..................................(6)
Equation (6) gives the total energy as a function orbit radius r.
 
To take a satellite from one orbit from other orbit we need to supply additional energy depends upon the radii of initial and final orbit.
Answered by Thiyagarajan K | 19 Jun, 2018, 05:30: PM
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