Derivation
Using energy conservation (set E_final = 0 at ∞):
Initial state (at surface): KE = ½mv_, PE = −GMm/R, Total = ½mv_ − GMm/R
Final state (at ∞, just barely): KE = 0, PE = 0, Total = 0
Energy conservation: ½mv_ − GMm/R = 0
v_e = =
Numerical Value for Earth
v_e = √(2 × 9.8 × $6.4 \times 10^{6}) = √(\1.2544 \times 10^{8}$) = 11,200 m/s = 11.2 km/s
Critical Independence Properties
v_e is independent of:
- Mass of projected body (m cancels in derivation)
- Angle of projection (energy approach has no direction dependence)
- Shape of escape trajectory (only energy at surface matters)
v_e depends on:
- Mass M of the planet (v_e ∝ √M)
- Radius R of the planet (v_e ∝ 1/√R)
Scaling Rule for Other Planets
v_e(planet) / v_e(Earth) = =
For same-density planets: (linear with radius)
Comparison with Other Planets
| Body | v_e (km/s) |
|---|---|
| Moon | 2.4 |
| Earth | 11.2 |
| Mars | 5.0 |
| Jupiter | 59.5 |
| Sun | 617.5 |
Why the Moon Has No Thick Atmosphere
Moon's escape velocity (2.4 km/s) is comparable to thermal velocities of gas molecules, so lighter gases escape over geological time.