AaronPrahst
- 14
- 0
He didn't tell us that.
The discussion revolves around determining the velocity of a communication satellite in circular orbit around the Earth at a height of 36,000 km. The problem is framed within the context of gravitational motion and involves Newton's law of gravitation, with specific constraints on the numerical values that can be used in the calculations.
Some participants have offered guidance on how to approach the problem using gravitational equations, while others express confusion about the constraints of the problem. There is an ongoing exploration of whether certain values can be used and how to interpret the problem's requirements.
Participants note that the problem explicitly states that only the radius of the Earth and the acceleration due to gravity at the surface can be used, leading to confusion about the relevance of the satellite's orbital height. There is also mention of the potential need for additional information, such as the orbital period of the satellite.
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...