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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 changeA. gravitational potential energyB. angular velocityC. linera orbital velocityD. centripetal acceleration |
Answer» Correct Answer - A `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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