An artificial satellite moving in a circular orbit around earth has a total energy E (potential energy +kinetic energy) it's potential energy is
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potential energy = total energy(E) - kinetic energy
mass × g(9.8) or (10) × height
mass × g(9.8) or (10) × height
ujjwala2:
answer in terms of E
(m×g×h) + 1\2×m×v×v
v is velocity
that is potential energy + kinetic energy
got it
could you send me the full solution
this was full solution
what is the answer
m×g×h + 1\2 ×m×v×v
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