1.

An earth satellite is movewd from one stable circular orbit to another larger and stable circular orbit. The following quantities increase for the satellite a result of this change

Answer»

gravitational potential energy
angular velocity
linera orbital velocity
centripetal acceleration

Solution :`U=-(GMm)/(R )` ltbRgt `OMEGA= sqrt((GM)/(r_(3)))`
`v= sqrt((GM)/(r )), a_(1) = r omega^(2)`
so only option (A) is CORRECT.


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