AaronPrahst
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He didn't tell us that.
The discussion centers on calculating the velocity of a communication satellite in circular orbit at 36,000 km above the Earth's surface using Newton's law of gravitation. Participants clarify that the only numerical values allowed are the Earth's radius and the acceleration due to gravity at the surface. The derived formula for velocity is v^2 = g * r_earth^2 / (r_earth + 36,000 * 10^3), where g is 9.8 m/s² and r_earth is 6,370,000 m. The final calculated velocity is approximately 3063.5 m/s.
PREREQUISITESStudents in physics courses, aerospace engineers, and anyone interested in satellite dynamics and gravitational physics.
D H said:The question said it was a communication satellite. Did your instructor tell you that communication satellites typically have an orbital period of 24 hours?
D H said:Your instructor must have told you something. Please write the problem exactly as it was given to you.
AaronPrahst said:Well thanks for trying to help us but I guess our teacher is just bad and we are screwed for now.
One question though I thought Gm1=(g at Re)timesRe^2
You just have down Gm1=(g at Re)^2
AaronPrahst said:Oh ok I understand that now sorry I just mis-read that.
Thanks again.
AaronPrahst said:Hmm well I plugged it in and got 1.32 m/s. Uh but I probably did something wrong...