Question #91057
a satellite is to be put into orbit 500km above the earths surface.if its vertical velocity after launching is 2000m/s at this height calculate the magnitude and direction of the impulse required to put the satellite directly into its orbit,if its mass is 50kg
1
Expert's answer
2019-06-24T09:30:09-0400
F=m×a=m×v2RF=m \times a=\frac{m \times v^2}{R}

F=G×m×MearthR2F=G \times \frac{m \times Mearth}{R^2}

Equalize these equations and find v:


v=(G×MR)12=7550meter/secv= (\frac{G \times M}{R})^\frac{1}{2}= 7550 meter/sec

Required speed to enter orbit 500 kilometers, at an initial velocity of 2000 meters per second, it will not enter a given orbit


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