Quick Recap — Advanced Gravitation (Multi-step)

  • Escape / orbital numbers: ve=2gRv_e=\sqrt{2gR}, vo=gRv_o=\sqrt{gR} (near surface); with g=10g=10, R=6.4×106R=6.4\times10^6 m these give 11.3\approx11.3 km/s and 8\approx8 km/s.
  • Scaling: gρRg\propto\rho R; veRρv_e\propto R\sqrt{\rho}; T2r3T^2\propto r^3 (Kepler).
  • Energy to raise a satellite from surface to orbit rr: ΔE=(GMm2r)(GMmR)\Delta E=\left(-\dfrac{GMm}{2r}\right)-\left(-\dfrac{GMm}{R}\right).
  • Speed to escape from an orbit (not the surface): v=2×v=\sqrt2\times(local orbital speed).

Worked mini-example. For g=10g=10, R=6.4×106R=6.4\times10^6 m: ve=2gR=1.28×1081.13×104v_e=\sqrt{2gR}=\sqrt{1.28\times10^8}\approx1.13\times10^4 m/s =11.3=11.3 km/s.