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
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
Kinetic energy K
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 ...........................(3)
from eqn.(3), after simplification, we get ......................(4)
By substituting for ω2r2 using eqn.(4) in eqn.(2), we get kinetic energy K = .................... (5)
Total energy U+K = ..................................(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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