hi i've got some qns that are confusing me
1. there was once a proposal to launch satelites directly into a circular orbit that's a constant distance from the earth, using a giant world war 1 cannon. assuming that the cannon could give the satelite a high enough velocity, explain why this proposal would not work.
2. if there is a question asking me to calculate the orbital velocity, do i use the formula "v=2pir/t" or "v=root of GM/r". becoz the 2nd one didnt specify the planet. or can i use both?
3. see attachment
Thanks in advance
1. there was once a proposal to launch satelites directly into a circular orbit that's a constant distance from the earth, using a giant world war 1 cannon. assuming that the cannon could give the satelite a high enough velocity, explain why this proposal would not work.
2. if there is a question asking me to calculate the orbital velocity, do i use the formula "v=2pir/t" or "v=root of GM/r". becoz the 2nd one didnt specify the planet. or can i use both?
3. see attachment
Thanks in advance