what conditions must be met if a man made satellite is to attain a circular orbit around the earth ? (choose as many as apply) (A) it must be launched with with a tangential speed of 0 (B) it must be launched with a tangential speed of 8 km/s (C) it must be launched with a tangential speed greater than 8 km/s (D) it must be launched horizontally at a distance over 150 kilometers above the earth (E) it must be launched vertically with a speed of 8 km/s i said d and a
Do you know what is tangential speed?
tangential speed is tangent to the way the object is moving
circular orbit: gravitational force = centripetal force to keep it in the circular orbit
minimum speed = \[\sqrt{gr}\] where r is the radius of the orbit. if its less, the object falls on the surface
im really confused :/
For Solving this Question, I would like to ask you that, do you have the detailed conception of : Satellite
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