How to Use This Page
1. Attempt every exercise question on your own — then verify your method and answer with the solutions below. 2. Memorise the key formulas — gravitation has many interrelated formulas; understanding the derivations helps you recall them. 3. Pay special attention to numerical problems — they are the highest-mark questions in the exam. 4. Review the Common Mistakes section — these are the most frequent errors in this chapter. 5. Use the Exam Checklist to ensure you have covered every concept before the exam.
Key Concepts (Quick Recap)
Newton's Universal Law of Gravitation
F = Gm₁m₂/r²
| Symbol | Meaning | SI Unit |
|---|
| F | Gravitational force | N |
| G | Universal gravitational constant = 6.674 × 10⁻¹¹ | N·m²/kg² |
| m₁, m₂ | Masses of two bodies | kg |
| r | Distance between centres | m |
Acceleration Due to Gravity
| Variation | Formula |
|---|
| On surface | g = GM/R² |
| At height h | g_h = GM/(R+h)² ≈ g(1 − 2h/R) for h << R |
| At depth d | g_d = g(1 − d/R) |
| At the centre | g = 0 |
| At poles vs equator | g_pole > g_equator (due to rotation and shape) |
Kepler's Laws of Planetary Motion
| Law | Statement | Formula |
|---|
| First (Law of orbits) | Planets move in elliptical orbits with the Sun at one focus | — |
| Second (Law of areas) | The radius vector sweeps equal areas in equal times | dA/dt = constant |
| Third (Law of periods) | T² ∝ r³ (for all planets around the same star) | T² = 4π²r³/GM |
Escape and Orbital Velocities
| Quantity | Formula | Value for Earth |
|---|
| Escape velocity | vₑ = √(2GM/R) = √(2gR) | ≈ 11.2 km/s |
| Orbital velocity (near surface) | vₒ = √(GM/R) = √(gR) | ≈ 7.9 km/s |
| Relation | vₑ = √2 × vₒ | vₑ ≈ 1.414 × vₒ |
Satellites
| Quantity | Formula |
|---|
| Orbital velocity | v = √(GM/r) = √(gR²/r) |
| Time period | T = 2π√(r³/GM) |
| Height of satellite | h = r − R |
| Geostationary orbit | h ≈ 36,000 km, T = 24 hr |
| Energy of satellite | KE = GMm/2r, PE = −GMm/r, TE = −GMm/2r |
Important Definitions
| Term | Definition |
|---|
| Gravitation | The force of attraction between any two bodies in the universe |
| Gravity | The force of attraction exerted by Earth on a body near its surface |
| Escape velocity | The minimum velocity needed for a body to escape a planet's gravitational field |
| Orbital velocity | The velocity of a satellite in a stable circular orbit |
| Weightlessness | The condition when the normal reaction is zero (e.g., in free fall or orbit) |
I. Choose the Best Answer (MCQs)
1. The value of G is 6.674 × 10⁻¹¹ N·m²/kg². If the distance between two bodies is doubled, the gravitational force becomes:
Answer
- (a) Doubled
- (b) Halved
- (c) One-fourth
- (d) Four times
Answer(c) One-fourth
ExplanationF ∝ 1/r². If r → 2r, F → F/4. Force is inversely proportional to the square of distance.
2. The acceleration due to gravity at a height equal to the radius of Earth (h = R) from the surface is:
Answer
- (a) g/4
- (b) g/2
- (c) g
- (d) 4g
Answer(a) g/4
Explanationg_h = GM/(R+h)² = GM/(R+R)² = GM/4R² = gR²/4R² = g/4.
3. The escape velocity from Earth is 11.2 km/s. The escape velocity from a planet with twice the radius and twice the mass of Earth is:
Answer
- (a) 11.2 km/s
- (b) 22.4 km/s
- (c) 7.9 km/s
- (d) 15.8 km/s
Answer(a) 11.2 km/s
Explanationvₑ = √(2GM/R). If M → 2M and R → 2R: vₑ' = √(2G × 2M/2R) = √(2GM/R) = vₑ = 11.2 km/s. The factor 2 cancels.
4. The time period of a satellite orbiting close to the Earth's surface is approximately:
Answer
- (a) 24 hours
- (b) 84.6 minutes
- (c) 12 hours
- (d) 90 minutes
Answer(b) 84.6 minutes
ExplanationT = 2π√(R³/GM) ≈ 2π√((6.4 × 10⁶)³/(6.674 × 10⁻¹¹ × 6 × 10²⁴)) ≈ 5063 s ≈ 84.4 minutes. Closest to 84.6 min.
5. Kepler's second law is a consequence of the conservation of:
Answer
- (a) Energy
- (b) Linear momentum
- (c) Angular momentum
- d) Mass
Answer(c) Angular momentum
ExplanationEqual areas in equal times implies L = mvr = constant, which is conservation of angular momentum.
6. If the radius of Earth were to shrink by 1% (mass unchanged), the value of g would:
Answer
- (a) Decrease by 1%
- (b) Increase by 2%
- (c) Decrease by 2%
- (d) Increase by 1%
Answer(b) Increase by 2%
Explanationg = GM/R². If R decreases by 1%, R' = 0.99R. g' = GM/(0.99R)² = GM/(0.9801R²) ≈ 1.02g. g increases by approximately 2%.
7. The total energy of a satellite in a circular orbit is:
Answer
- (a) Positive
- (b) Zero
- (c) Negative
- (d) Cannot be determined
Answer(c) Negative
ExplanationTE = −GMm/2r. The total energy is negative, meaning the satellite is bound to the planet. Energy must be supplied to escape.
II. Fill in the Blanks
1. The universal gravitational constant G has the value ________ N·m²/kg². 6.674 × 10⁻¹¹ 2. The acceleration due to gravity at the centre of the Earth is ________. Zero 3. The escape velocity from a planet depends on its ________ and ________. Mass, radius 4. Kepler's first law states that planets move in ________ orbits. Elliptical 5. The relation between escape velocity and orbital velocity is vₑ = ________. √2 × vₒ 6. The value of g at the equator is ________ than at the poles. Less 7. The time period of a geostationary satellite is ________ hours. 24 8. If the mass of Earth were doubled and radius halved, the value of g would become ________ times. 8 9. The weight of a body in a freely falling lift is ________. Zero (weightlessness) 10. The orbital velocity of a satellite close to Earth's surface is approximately ________ km/s. 7.9 11. The gravitational force between two bodies is always ________ (attractive/repulsive). Attractive 12. The potential energy of a satellite is always ________ (positive/negative). Negative
III. True or False (with corrections)
1. The value of G changes with the distance between the bodies.
- False. G is a universal constant; its value (6.674 × 10⁻¹¹ N·m²/kg²) is the same everywhere in the universe and does not depend on the medium or distance.
2. The value of g is the same at all places on the surface of the Earth.
- False. g varies with latitude (maximum at poles, minimum at equator), altitude, and depth. It also varies with local geology.
3. A geostationary satellite can be placed at any latitude.
- False. A geostationary satellite must orbit in the equatorial plane, so it appears stationary relative to Earth. It cannot be placed at any latitude other than the equator.
4. Escape velocity depends on the mass of the escaping body.
- False. vₑ = √(2GM/R) depends on the mass M and radius R of the planet, not on the mass of the body escaping. A feather and a heavy rocket need the same escape velocity from the same planet.
5. If Earth stops rotating, the value of g at the equator would increase.
- True. The centrifugal effect due to rotation reduces g at the equator. If rotation stops, this reduction vanishes and g increases at the equator.
IV. Match the Following
| Column A | Column B |
|---|
| 1. g on surface | (e) GM/R² |
| 2. g at height h | (a) g(1 − 2h/R) |
| 3. g at depth d | (d) g(1 − d/R) |
| 4. Escape velocity | (f) √(2GM/R) |
| 5. Orbital velocity | (b) √(GM/R) |
| 6. Time period of satellite | (c) 2π√(r³/GM) |
V. Answer Briefly (2-mark Questions)
1. State Kepler's three laws of planetary motion.
Answer
First law (Law of orbits): Every planet moves in an elliptical orbit with the Sun at one of the foci. Second law (Law of areas): The radius vector joining a planet to the Sun sweeps out equal areas in equal intervals of time. Third law (Law of periods): The square of the time period of revolution is proportional to the cube of the semi-major axis: T² ∝ r³.
2. Why is g greater at the poles than at the equator?
Answer
Two reasons: (1) Earth is not a perfect sphere — it is an oblate spheroid with greater radius at the equator. Since g = GM/R², a larger R means smaller g at the equator. (2) The centrifugal effect due to Earth's rotation reduces the effective g at the equator more than at the poles. Both effects make g approximately 9.83 m/s² at the poles and 9.78 m/s² at the equator.
3. What is weightlessness? When does a body experience it?
Answer
Weightlessness is the condition in which a body experiences no normal reaction force, making it feel as if it has no weight. This occurs in: (1) a freely falling lift or elevator (g_eff = 0), (2) an orbiting satellite (both the satellite and the person inside are in free fall together), and (3) at the centre of the Earth (g = 0). The body still has mass and is still acted upon by gravity, but the apparent weight is zero.
4. Distinguish between g and G.
Answer
| Property | g | G |
|---|
| Full name | Acceleration due to gravity | Universal gravitational constant |
| Value | ~9.8 m/s² (varies) | 6.674 × 10⁻¹¹ N·m²/kg² (constant) |
| Depends on | Mass and radius of planet, altitude, latitude | Nothing (universal constant) |
| Nature | Vector | Scalar |
VI. Answer in Detail (5-mark Questions with Numerical Examples)
1. State Newton's law of gravitation and derive the expression for acceleration due to gravity. Show how g varies with altitude and depth. Solve: Calculate the acceleration due to gravity at a height of 100 km and at a depth of 100 km from the surface of Earth (R = 6400 km, g = 9.8 m/s²).
Answer
Statement: Every particle of matter attracts every other particle with a force that is proportional to the product of their masses and inversely proportional to the square of the distance between them: F = Gm₁m₂/r².
Derivation of g: For a body of mass m on Earth's surface (radius R, mass M): F = GMm/R² = mg → g = GM/R²
Variation with altitude (h): g_h = GM/(R+h)² = gR²/(R+h)² ≈ g(1 − 2h/R) for h << R
Variation with depth (d): At depth d, the mass of the shell of thickness d exerts no net force (shell theorem). Only mass within radius (R−d) contributes: g_d = G × M_enclosed / (R−d)² = G × M(R−d)³/(R³(R−d)²) = GM(R−d)/R³ = g(1 − d/R)
Numerical:
Given: R = 6400 km, g = 9.8 m/s², h = d = 100 km
(a) At height h = 100 km:
g_h = g × R² / (R + h)²
= 9.8 × (6400)² / (6400 + 100)²
= 9.8 × (6400/6500)²
= 9.8 × (6400/6500)²
= 9.8 × (0.9846)²
= 9.8 × 0.9695
≈ 9.5 m/s²
Using approximation: g_h ≈ g(1 − 2h/R) = 9.8(1 − 200/6400)
= 9.8(1 − 0.03125) = 9.8 × 0.9688 ≈ 9.49 m/s²
(b) At depth d = 100 km:
g_d = g(1 − d/R) = 9.8(1 − 100/6400)
= 9.8(1 − 0.015625)
= 9.8 × 0.984375
≈ 9.65 m/s²
Answer: g at 100 km height ≈ 9.50 m/s²
g at 100 km depth ≈ 9.65 m/s²
2. Define escape velocity and derive its expression. Also derive orbital velocity. Solve: Calculate the escape velocity and orbital velocity near Earth's surface. Given: M = 6 × 10²⁴ kg, R = 6.4 × 10⁶ m, G = 6.674 × 10⁻¹¹ N·m²/kg².
Answer
Derivation of escape velocity: For a body of mass m to escape a planet of mass M and radius R, its KE must at least equal the gravitational PE at the surface.
½mvₑ² = GMm/R
vₑ = √(2GM/R)
Since g = GM/R² → GM = gR²: vₑ = √(2gR)
Derivation of orbital velocity: For a satellite in circular orbit at radius r, gravitational force provides centripetal force: GMm/r² = mv²/r
vₒ = √(GM/r)
For orbit near Earth's surface (r ≈ R): vₒ = √(GM/R) = √(gR)
Relation: vₑ = √2 × vₒ (escape velocity is √2 times orbital velocity)
Numerical:
Given: M = 6 × 10²⁴ kg, R = 6.4 × 10⁶ m, G = 6.674 × 10⁻¹¹
Escape velocity:
vₑ = √(2GM/R)
= √(2 × 6.674 × 10⁻¹¹ × 6 × 10²⁴ / 6.4 × 10⁶)
= √(8.0088 × 10¹⁴ / 6.4 × 10⁶)
= √(1.2514 × 10⁸)
≈ 11,187 m/s
≈ 11.2 km/s
Orbital velocity (near surface):
vₒ = √(GM/R)
= √(6.674 × 10⁻¹¹ × 6 × 10²⁴ / 6.4 × 10⁶)
= √(4.0044 × 10¹⁴ / 6.4 × 10⁶)
= √(6.2569 × 10⁷)
≈ 7,910 m/s
≈ 7.9 km/s
Verification: vₑ/vₒ = 11.2/7.9 = 1.414 = √2 ✓
Answer: Escape velocity ≈ 11.2 km/s
Orbital velocity ≈ 7.9 km/s
3. Derive the expression for the time period and energy of a satellite. Solve: A satellite orbits Earth at a height of 400 km. Find its orbital velocity, time period, and total energy per unit mass. Given: M = 6 × 10²⁴ kg, R = 6.4 × 10⁶ m.
Answer
Derivation of time period: For a satellite in circular orbit at radius r: v = √(GM/r)
Time period T = distance/speed = 2πr/v = 2πr/√(GM/r)
T = 2π√(r³/GM)
This is Kepler's third law: T² = 4π²r³/GM.
Energy of satellite: KE = ½mv² = ½m × GM/r = GMm/2r PE = −GMm/r (gravitational PE, negative by convention) TE = KE + PE = GMm/2r − GMm/r = −GMm/2r
Numerical:
Given: h = 400 km = 4 × 10⁵ m, R = 6.4 × 10⁶ m
r = R + h = 6.4 × 10⁶ + 4 × 10⁵ = 6.8 × 10⁶ m
M = 6 × 10²⁴ kg, G = 6.674 × 10⁻¹¹
(a) Orbital velocity:
v = √(GM/r) = √(6.674 × 10⁻¹¹ × 6 × 10²⁴ / 6.8 × 10⁶)
= √(4.004 × 10¹⁴ / 6.8 × 10⁶)
= √(5.888 × 10⁷)
≈ 7674 m/s ≈ 7.67 km/s
(b) Time period:
T = 2πr/v = 2π × 6.8 × 10⁶ / 7674
= 2 × 3.1416 × 6.8 × 10⁶ / 7674
= 42.73 × 10⁶ / 7674
≈ 5567 s
≈ 92.8 minutes
Verification: T = 2π√(r³/GM)
= 2π√((6.8 × 10⁶)³/(6.674 × 10⁻¹¹ × 6 × 10²⁴))
≈ 5567 s ✓
(c) Total energy per unit mass:
TE/m = −GM/2r
= −6.674 × 10⁻¹¹ × 6 × 10²⁴ / (2 × 6.8 × 10⁶)
= −4.004 × 10¹⁴ / (1.36 × 10⁷)
= −2.944 × 10⁷ J/kg
≈ −29.44 MJ/kg
Answer: Orbital velocity ≈ 7.67 km/s
Time period ≈ 92.8 minutes
Total energy per unit mass ≈ −29.44 MJ/kg
Common Mistakes to Avoid
1. Confusing G and g — G (6.674 × 10⁻¹¹ N·m²/kg²) is a universal constant; g (≈ 9.8 m/s²) is the acceleration due to gravity on Earth's surface and varies with location.
2. Forgetting to add height to Earth's radius — for a satellite at height h, the orbital radius is r = R + h, not just h. Always use r = R + h in orbital formulas.
3. Sign errors in potential energy — gravitational PE is negative (PE = −GMm/r). The total energy TE = −GMm/2r is also negative for bound orbits. A positive total energy means the body is not bound.
4. Using g = 9.8 m/s² at all altitudes — g decreases with altitude. Use g_h = GM/(R+h)² or the approximation g(1 − 2h/R) for h << R.
5. Not converting units — distances in km must be converted to m before using in formulas with G. Heights given in km → multiply by 10³.
6. Mixing up escape and orbital velocities — vₑ = √(2GM/R) and vₒ = √(GM/R). Remember vₑ = √2 × vₒ. They are not the same.
7. Applying depth formula for altitude (or vice versa) — for altitude: g_h ≈ g(1 − 2h/R); for depth: g_d = g(1 − d/R). These are different formulas.
8. Forgetting that gravitational force is always attractive — it can never be repulsive. The negative sign in PE indicates attraction, not repulsion.
Exam Checklist
- [ ] Can state Newton's law of gravitation and derive g = GM/R²
- [ ] Know how g varies with altitude (g_h ≈ g(1 − 2h/R)) and depth (g_d = g(1 − d/R))
- [ ] Can state and explain all three of Kepler's laws
- [ ] Can derive escape velocity (vₑ = √(2GM/R)) and orbital velocity (vₒ = √(GM/r))
- [ ] Know the relation vₑ = √2 × vₒ and can derive it
- [ ] Can calculate time period of a satellite (T = 2π√(r³/GM))
- [ ] Know the energy of a satellite: KE = GMm/2r, PE = −GMm/r, TE = −GMm/2r
- [ ] Can explain weightlessness and when it occurs
- [ ] Remember unit conversions (km to m) and G = 6.674 × 10⁻¹¹ N·m²/kg²
- [ ] Can explain why g is greater at poles than at equator (shape + rotation)