Gravitation
Kepler's three laws, Newton's universal gravitation & Cavendish G, variation of g with altitude & depth, potential energy, escape speed & satellites.
Topic 7.2: Kepler's Three Laws of Planetary Motion
ΔA/Δt = L/(2m) = constant (Consequence of angular momentum conservation!)T² ∝ a³ (Square of year ∝ Cube of semi-major axis a)- 1First Law (Law of Orbits): All planets move in elliptical orbits with the Sun situated at one of the two foci (semi-major axis
a = (rmin + rmax)/2). - 2Second Law (Law of Areas): The line joining any planet to the Sun sweeps equal areas in equal intervals of time:
ΔAΔt = L2m = constant. Why? Gravity acts straight toward the Sun, so torqueτ = r × F = 0and angular momentumLis conserved! - 3Third Law (Law of Periods): Square of revolution time period is proportional to cube of semi-major axis:
T² = (4π²GMs) a³⇒(T₁/T₂)² = (a₁/a₂)³!
4 times farther from the Sun than Earth (a₂ = 4 a₁), its year takes T₂ = 43/2 = 8 Earth years!
L — because central gravitational force exerts ZERO torque about the Sun!Topic 7.3 – 7.4: Newton's Universal Law & Cavendish Experiment
F = G m₁ m₂r² (Always attractive, central & inverse-square!)G = 6.67 × 10⁻¹¹ N·m²/kg² • Dim: [M⁻¹L³T⁻²]G is Universal (NEVER changes anywhere!), whereas g is Local (changes by planet/height)!G = 0.0000000000667 is so unimaginably tiny that you need planet-sized mass to notice the tug!- 1Inverse-Square Vector Law: Every pair of point masses attract along the line joining them:
F₁₂ = −G m₁m₂r² r̂₂₁. Force forms an equal & opposite Newton's 3rd Law pair and obeys superposition for multiple masses! - 2Shell Theorem: A uniform spherical shell pulls any outside particle as if all mass sat at the centre, yet pulls ZERO on any particle anywhere inside the hollow shell!
- 3Cavendish Torsion Balance (1798): Using tiny lead spheres twisted on a thin quartz fibre, Henry Cavendish measured
G = 6.67 × 10⁻¹¹ N·m²/kg²— which instantly let scientists "weigh" the Earth:ME = gRE² / G ≈ 6 × 10²⁴ kg!
160 N at separation r. If moved to 2r, force drops by 2² = 4 times → 160 / 4 = 40 N!
G change on the Moon or underwater? NO! G is universal and medium-independent (unlike electrostatic Coulomb's constant!). (2) Gravitational force inside a uniform hollow spherical shell is ZERO everywhere inside! (3) Doubling distance cuts force to one-fourth, NOT half.Topic 7.5 – 7.6: Acceleration due to Gravity g with Altitude & Depth
g = 0 and you float weightless!g = GMR² = 43 π G R ρ ≈ 9.8 m/s²g(h) = g(1 + h/R)² | For h ≪ R: g(h) ≈ g(1 − 2hR)g(d) = g(1 − dR) (Exact linear drop; at centre d=R ⇒ g=0!)g peaks right on Earth's surface and drops BOTH when you climb up (−2h/R, 2× faster!) AND dig down (−d/R)!d, the outer shell of thickness d above your head pulls ZERO net force (by Shell Theorem!), so only the smaller inner core of radius (R − d) pulls you!- 1Why Heavy & Light Stones Fall Together: Setting
mg = GMm/R²cancels the falling object's massm! Sog = GM / R²depends ONLY on the planet's mass & radius. - 2Going UP (Altitude
h): Distance from Earth's centre becomesR + h, sog(h) = g R² / (R + h)². For small heights (h ≪ R), binomial expansion givesg(h) ≈ g(1 − 2h/R)! (Note: ath = R,gdrops tog/4!). - 3Going DOWN (Depth
d): Only inner sphere of radiusr = R − dpulls, whose mass shrinks asr³while distance squared isr²→ net pull scales linearly withr! Thusg(d) = g(1 − d/R)! At Earth's centre (d = R),g = 0!
1% of Earth's radius up (h = R/100) cuts g by 2%, while digging 1% down (d = R/100) cuts g by only 1%! To match a drop at small altitude h, you must dig twice as deep (d = 2h)!
g → ∞ as you approach Earth's centre (r → 0)! Wrong — inside a solid sphere, g ∝ r rises linearly from 0 at centre to maximum 9.8 m/s² at surface, then falls as 1/r² outside! (2) Remember for small heights, g decreases twice as fast with height h as with depth d (d = 2h gives same g)!Topic 7.7: Gravitational Potential Energy
U(r) = −GMmr (Reference U(∞) = 0; always negative!)ΔU = U(R+h) − U(R) = mgh1 + h/RV(r) = U/m = −GMr (Scalar; SI unit: J/kg)U = −GMm/r has ONE power of r (unlike Force 1/r²), and Minus means Bound in Earth's Gravity Well!mgh for rockets? Because mgh assumes gravity stays 9.8 all the way up! For high rockets, gravity weakens with distance, so lifting a satellite by a whole Earth radius (h = R) costs only half as much energy as mgR!- 1Why
U(r)is Negative: ChoosingU = 0at infinite separation (where gravitational pull fades to zero), since gravity is attractive, bringing massmfrom∞to distancerreleases energy, leavingU(r) = −GMm / r! - 2Work Done Lifting from Surface (
R) to Height (R + h):ΔU = −GMmR + h − (−GMmR) = GMmhR(R+h) = mgh1 + h/R! - 3Connecting Back to
mgh: Whenh ≪ R(like tossing a ball or climbing stairs),h/R ≈ 0soΔUsmoothly simplifies tomgh!
m from Earth's surface to height h = R:Plug
h = R into mgh / (1 + h/R) → mgR / (1 + 1) = ½ mgR (NOT mgR)!
m from Earth's surface to height h = R (or 2R). Students blindly plug mgh = mgR and get zero marks! You MUST use ΔU = mgh / (1 + h/R) → giving ½ mgR for h = R (and ⅔ mgR for h = 2R)!Topic 7.8: Escape Speed from Earth (and Planets)
11.2 km/s, and it climbs completely out of Earth's potential well — never falling back again!ve = √(2GMR) = √(2gR)11.2 km/s • Moon: 2.38 km/s (lost air!)m & launch angle!½mve² = +GMm/R (exact debt) ⇒ mass m cancels cleanly out!11.2 km/s — because projectile mass m cancels from both sides!- 1Energy Conservation Derivation: Launch at minimum speed
veso rocket reaches∞withK∞ = 0, U∞ = 0:½ m ve² − GMmR = 0 ⇒ ve = √(2GMR) = √(2gR)(sinceGM = gR²). - 2Earth & Moon Comparison: Plugging Earth's
g = 9.8 m/s², R = 6.4 × 10⁶ mgivesve ≈ 11.2 km/s. Moon's tinyve ≈ 2.3 km/sis slower than warm gas molecules, so the Moon's air escaped into space! - 3Launching Faster than
ve: If thrown withv > ve, remaining speed at infinity comes from energy conservation:½mv∞² = ½mv² − ½mve² ⇒ v∞ = √(v² − ve²)!
m of the rocket or the angle of launch (neglecting air drag)! (2) Why is it called escape speed and not velocity? Because direction doesn't matter! (3) If projected at v = 2ve, speed at infinity is √(4ve² − ve²) = √3 ve (NOT ve!).Topic 7.9 – 7.10: Earth Satellites, Orbital Speed & Total Energy
400 km altitude, gravity still pulls at ~90% of its surface strength! The satellite simply flies sideways so fast (~7.9 km/s) that as it falls toward Earth, Earth curves away beneath it!vo = √(GMR+h) • Near Earth: vo = √(gR) ≈ 7.92 km/s • ve = √2 vo!T = 2π √((R+h)³GM) (Near Earth ≈ 85 min)K = +GMm2r | U = −GMmr | E = −GMm2r = −K = U/2E = −K & U = 2E! Check signs: K is positive (+1), E is negative (−1), and U is double negative (−2) — so +1 + (−2) = −1!N = 0)!- 1Orbital Speed Derivation: Gravity supplies the exact centripetal force needed for circular orbit of radius
r = R + h:mvo²r = GMmr² ⇒ vo = √(GMR+h). Right near Earth (h ≪ R),vo = √(gR) ≈ 7.92 km/s, sove = √2 vo! - 2Orbit Time Period:
T = 2πrvo = 2π √(r³GM)(matches Kepler's 3rd lawT² ∝ r³!). Close to Earth's surface,T₀ = 2π√(R/g) ≈ 85 minutes. - 3Energy of an Orbiting Satellite: Kinetic
K = ½mvo² = +GMm2r; PotentialU = −GMmr; TotalE = K + U = −GMm2r. Negative total energy means the satellite is bound to Earth!
r ↓) — what happens to its orbital speed vo and kinetic energy K? They actually INCREASE (E = −K becomes more negative, so K goes UP while U drops twice as much)! (2) Weightlessness in orbit happens due to free fall (zero normal reaction), NOT zero gravity!Solved Previous Year Questions (Kerala DHSE & NCERT)
Q1 (Kerala HSE March • 2 Marks): State Kepler's Second and Third Laws of planetary motion. Which physical conservation law underlies the Second Law?
ΔA/Δt = constant). It is based on Conservation of Angular Momentum (L = 2m ΔA/Δt, zero central torque).• Law of Periods (3rd): Square of orbital time period is proportional to cube of semi-major axis:
T² ∝ a³.Q2 (Kerala HSE Say • 1 Marks): Does the universal gravitational constant G depend on the nature of the medium between two masses or on location (Earth vs Moon)? Write its dimensional formula.
G = 6.67 × 10⁻¹¹ N·m²/kg² is truly universal and independent of medium or planet.Dimensional formula:
[G] = [F r² / m²] = [MLT⁻²][L²]/[M²] = [M⁻¹ L³ T⁻²].Q3 (Kerala HSE March • 3 Marks): Derive an expression for acceleration due to gravity at a depth d below the Earth's surface. What happens to g at the centre of the Earth?
ρ, surface g = (4/3)π G R ρ.At depth
d (distance r = R − d from centre), the outer shell exerts zero force; only inner sphere of radius (R − d) pulls:g(d) = (4/3)π G (R − d) ρ = g (1 − d/R).At Earth's centre (
d = R), g(R) = g(1 − 1) = 0 (weightless!).Q4 (Kerala HSE Model • 3 Marks): Derive the variation of acceleration due to gravity g with altitude h above Earth's surface (for both general h and small h ≪ R).
h, g(h) = GM / (R + h)². Dividing by g = GM / R²:g(h) = g / (1 + h/R)² = g(1 + h/R)⁻².For
h ≪ R, binomial expansion gives g(h) ≈ g (1 − 2h/R).Q5 (Kerala HSE March • 2 Marks): At what height above Earth's surface is the value of g the same as at a depth of 80 km below the surface? (Assume h, d ≪ R)
g(1 − 2h/R) = g(1 − d/R) ⇒ 2h = d.Thus
h = d / 2 = 80 / 2 = 40 km.Q6 (Kerala HSE Say • 2 Marks): Calculate the work done in lifting a body of mass m from the surface of the Earth (radius R) to a height equal to R.
ΔU = U(2R) − U(R):ΔU = −GMm/(2R) − (−GMm/R) = +GMm/(2R).Since
GM = gR², ΔU = ½ mgR!Q7 (Kerala HSE March • 3 Marks): Define Escape Speed. Derive an expression for escape speed from Earth's surface and calculate its value (g = 9.8 m/s², R = 6.4 × 10⁶ m).
By energy conservation:
½mve² − GMm/R = 0 ⇒ ve = √(2GM/R) = √(2gR).Calculation:
ve = √(2 × 9.8 × 6.4 × 10⁶) ≈ 11.2 km/s.Q8 (Kerala HSE Model • 3 Marks): Derive the expressions for Orbital Speed, Kinetic Energy, Potential Energy, and Total Energy of a satellite of mass m orbiting Earth at radius r = R + h. What does the negative sign in Total Energy signify?
mvo²/r = GMm/r² ⇒ vo = √(GM/r).• Kinetic:
K = ½mvo² = +GMm / (2r)• Potential:
U = −GMm / r• Total Energy:
E = K + U = −GMm / (2r) = −K.The negative sign signifies that the satellite is gravitationally bound to Earth.