The relative uncertainty in the period of a satellite orbiting around the earth is 10⁻⁶. If the relative uncertainty in the radius of the orbit is negligible, the relative uncertainty in the mass of the earth is :
10⁻⁶
3×10⁻⁶
6×10⁻⁶
2×10⁻⁶
Solution:
The correct option is C 2×10⁻⁶ Time period,T=2π√(r³/GM) Squaring om both sides,T²=4(π)²r³/GM Taking log,ln(T²)=ln(4(π)²r³/GM) ln(T²)=ln(4(π)²r³G)-ln(M) 2ln(T)=ln(K)-ln(M) 2ΔT/T=ΔM/M ΔM/M=2×10⁻⁶