pureouchies4717
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i solved it. thanks to all who responded
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The discussion revolves around understanding the dynamics of satellites in orbit, specifically focusing on the energy conservation principles and velocity calculations for a satellite transitioning between orbits.
Some participants have provided insights into energy conservation and velocity calculations, while others express uncertainty about the relationship between different orbital speeds. The conversation reflects a mix of confirmations and requests for clarification without reaching a definitive consensus.
Participants are discussing a specific scenario involving a 1000 kg communication satellite and its required velocity for transitioning to a geosynchronous orbit, with some constraints implied by homework guidelines.
Can you show how you got that answer?nick727kcin said:a.)Consider a 1000 kg communication satellite that needs to be boosted from an orbit 300 km above the Earth to a geosynchronous orbit 35,900 km above the earth. Find the velocity v_1 on the lower circular orbit.
this came out to be: 7730m/s
nick727kcin said:thanks for responding guys, and i got that answer by using this formula:
v= (sq. root) GM/(Re+h)
part a is definitely right, though