Physics by Lamhi: Not Your Boring Physics

CLASS 11 · CHAPTER 7 · MECHANICS

QUICK REVISION

Gravitation

Every key result from this chapter, boxed and ready for a last look before the exam. No derivations here, just what to recall and when to use it — for the full explanation, see the detailed notes.

1. Kepler's Three Laws

  1. First law (orbits): every planet moves in an ellipse, Sun at one focus.
  2. Second law (areas): the Sun–planet line sweeps equal areas in equal times — angular momentum about the Sun stays constant.
  3. Third law (periods): T2∝a3T^2 \propto a^3, same constant for every planet around the Sun.

2. Newton's Universal Law of Gravitation

Universal law of gravitation
F=Gm1m2r2F = \dfrac{Gm_1m_2}{r^2}

G=6.674×10−11 N m2kg−2G = 6.674\times10^{-11}\ \text{N m}^2\text{kg}^{-2} — always attractive, always inverse-square.

Reproduces Kepler's third law
T2=(4π2GM)r3T^2 = \left(\dfrac{4\pi^2}{GM}\right)r^3

3. g — Variation with Height and Depth

g at the surface
g=GMR2g = \dfrac{GM}{R^2}
  1. Height h (h≪R): g(h)≈g(1−2hR)g(h) \approx g\left(1-\dfrac{2h}{R}\right) — falls off twice as fast per metre as depth.
  2. Depth d: g(d)=g(1−dR)g(d) = g\left(1-\dfrac{d}{R}\right) — a straight line, zero at the centre.

4. Gravitational P.E. and Escape Speed

Gravitational P.E.
U(r)=−GMmrU(r) = -\dfrac{GMm}{r}
Escape speed
ve=2GMRv_e = \sqrt{\dfrac{2GM}{R}}

Independent of launched mass mm and of launch direction — only launch speed matters.

5. Orbital Velocity and Satellite Energy — the −K, U/2 Pattern

Orbital velocity
vorbital=GMrv_{\text{orbital}} = \sqrt{\dfrac{GM}{r}}
K=GMm2rU=−GMmrE=K+U=−GMm2r=−K=U2K = \dfrac{GMm}{2r} \qquad U = -\dfrac{GMm}{r} \qquad E = K+U = -\dfrac{GMm}{2r} = -K = \dfrac{U}{2}

Every bound circular orbit: total energy negative, equals −K-K, equals U/2U/2 — for any rr, mm, or MM.

6. Orbit Type by Launch Speed

ve=2×vorbitalv_e = \sqrt{2}\times v_{\text{orbital}}
  1. Launch speed = vorbitalv_{\text{orbital}}: circular orbit.
  2. Between vorbitalv_{\text{orbital}} and vev_e: elliptical (bound) orbit.
  3. At or above vev_e (= 2 vorbital\sqrt{2}\,v_{\text{orbital}}): orbit opens up — a one-way escape, not a closed path.

7. Geostationary Orbits, Polar Satellites, and Weightlessness

Geostationary radius condition
r=(GMT24π2)1/3r = \left(\dfrac{GMT^2}{4\pi^2}\right)^{1/3}
  1. Geostationary: equatorial plane + west-to-east + T=24 hT=24\text{ h} → one unique rr (altitude ≈ 35,900 km).
  2. Polar: low altitude, period ≈ 100 min, passes near both poles — images the whole planet over many orbits.
  3. Weightlessness: satellite and contents in free fall together — normal force vanishes, scale reads zero.

Full derivations and worked examples: detailed notes →