Gravitation (Calculus-Based)

AP Physics C Mechanics study guide for gravitation: universal law of gravity, gravitational potential energy, orbits, escape speed, and Kepler's laws.

# Gravitation (Calculus-Based) — AP Physics C Mechanics

AP Physics C covers gravitation with full use of calculus, including deriving gravitational potential energy, analyzing orbits, and computing escape velocity. This topic connects Newton's laws to planetary and satellite motion.

Key Concepts

Newton's Law of Universal Gravitation

F=GMmr2r^F = -\frac{GMm}{r^2}\hat{r} (Negative sign: force is attractive, directed inward.)

Gravitational Field

g=GMr2r^\vec{g} = -\frac{GM}{r^2}\hat{r}

Inside a uniform spherical shell: g=0g = 0.

Inside a solid sphere at radius r<Rr < R: g=GMrr2g = \frac{GM_r}{r^2} where Mr=M(r/R)3M_r = M(r/R)^3, so g=GMrR3g = \frac{GMr}{R^3}.

Gravitational Potential Energy

U=GMmrU = -\frac{GMm}{r}

Derived from: U=rFdr=rGMmr2drU = -\int_\infty^r F\,dr' = -\int_\infty^r \frac{GMm}{r'^2}\,dr'.

Reference: U=0U = 0 at r=r = \infty.

Escape Speed

Total energy = 0 at escape: 12mve2GMmR=0\frac{1}{2}mv_e^2 - \frac{GMm}{R} = 0 ve=2GMRv_e = \sqrt{\frac{2GM}{R}}

Orbits

Circular orbit: v=GMr,T2=4π2GMr3v = \sqrt{\frac{GM}{r}}, \quad T^2 = \frac{4\pi^2}{GM}r^3

Total energy in orbit: E=KE+U=12mv2GMmr=GMm2rE = KE + U = \frac{1}{2}mv^2 - \frac{GMm}{r} = -\frac{GMm}{2r}

  • Bound orbit: E<0E < 0.
  • Escape: E0E \geq 0.

Kepler's Laws

  1. Planets orbit in ellipses with the Sun at one focus.
  2. A line from the Sun to a planet sweeps equal areas in equal times (conservation of angular momentum).
  3. T2a3T^2 \propto a^3 where aa is the semi-major axis.

Worked Example

Problem: Find the escape speed from Earth's surface. (ME=5.97×1024 kgM_E = 5.97 \times 10^{24}\ \text{kg}, RE=6.37×106 mR_E = 6.37 \times 10^6\ \text{m})

Solution:

ve=2GMR=2(6.674×1011)(5.97×1024)6.37×106v_e = \sqrt{\frac{2GM}{R}} = \sqrt{\frac{2(6.674 \times 10^{-11})(5.97 \times 10^{24})}{6.37 \times 10^6}} =7.97×10146.37×106=1.25×10811,200 m/s11.2 km/s= \sqrt{\frac{7.97 \times 10^{14}}{6.37 \times 10^6}} = \sqrt{1.25 \times 10^8} \approx 11{,}200\ \text{m/s} \approx 11.2\ \text{km/s}

Practice Questions

  1. 1. A satellite orbits Earth at radius 2RE2R_E. What is its orbital speed in terms of gg and RER_E?

    v=GM/(2RE)v = \sqrt{GM/(2R_E)}. Since g=GM/RE2g = GM/R_E^2, GM=gRE2GM = gR_E^2. v=gRE2/(2RE)=gRE/2v = \sqrt{gR_E^2/(2R_E)} = \sqrt{gR_E/2}.

    2. What is the total energy of a 100 kg100\ \text{kg} satellite in a circular orbit at altitude h=REh = R_E above Earth's surface?

    r=2REr = 2R_E. E=GMm/(2r)=gRE2m/(22RE)=mgRE/4=(100)(9.8)(6.37×106)/41.56×109 JE = -GMm/(2r) = -gR_E^2 m/(2 \cdot 2R_E) = -mgR_E/4 = -(100)(9.8)(6.37 \times 10^6)/4 \approx -1.56 \times 10^9\ \text{J}.

    3. Derive that gravitational potential energy U=GMm/rU = -GMm/r by integrating the gravitational force from infinity to rr.

    U=r(GMmr2)dr=GMmrdrr2=GMm[1/r]r=GMm(1/r0)=GMm/rU = -\int_\infty^r \left(-\frac{GMm}{r'^2}\right)dr' = GMm \int_\infty^r \frac{dr'}{r'^2} = GMm[-1/r']_\infty^r = GMm(-1/r - 0) = -GMm/r.

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Summary

  • U=GMm/rU = -GMm/r with U=0U = 0 at infinity.
  • Escape speed: ve=2GM/Rv_e = \sqrt{2GM/R}.
  • Circular orbit: v=GM/rv = \sqrt{GM/r}, E=GMm/(2r)E = -GMm/(2r).
  • Kepler's second law is conservation of angular momentum.
  • Inside a uniform sphere, grg \propto r; inside a shell, g=0g = 0.

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