⭐ Gravitation — At a Glance
9.8
g on Earth (m/s²)
6.67×10⁻¹¹
G (Nm²/kg²)
11.2
Escape Vel. Earth (km/s)
8
Orbital Vel. (km/s)
  • Gravitation = Force of attraction between any two bodies in the universe
  • Proponent: Isaac Newton
  • Universal Gravitational Constant G discovered by Cavendish (1798)
  • Key topics: Newton's Law · g variation · Kepler's Laws · Satellites · Escape Velocity
📌 Key Formulas
F = G(m₁m₂) / r²Newton's Gravitational Force
g = GMₑ / Rₑ²Gravitational Acceleration
Vₒ = √(gR)Orbital Velocity
Vₑ = √(2gR)Escape Velocity
🗂️ Chapter Topics
  • Newton's Universal Law of Gravitation
  • Gravitational Constant (G) vs Acceleration (g)
  • Change in value of g (altitude, depth, latitude)
  • Kepler's 3 Laws of Planetary Motion
  • Mass vs Weight
  • Satellites & Geostationary Orbit
  • Escape Velocity
🍎 Newton's Universal Law of Gravitation
📘 Definition

Every object in the universe attracts every other object with a force that is directly proportional to the product of their masses and inversely proportional to the square of the distance between them.

F ∝ m₁ × m₂ / r² Proportional form
F = G × (m₁ × m₂) / r² Full formula with G
🔢 Gravitational Constant (G)
  • Symbol: G
  • Value: 6.67 × 10⁻¹¹ Nm²/kg²
  • Discovered by: Henry Cavendish (1798)
  • Universal constant — same everywhere in universe
  • Does NOT change with location or mass
⚠️ Exam Trap

G (Gravitational Constant) ≠ g (Gravitational Acceleration). G is universal & fixed; g changes with location.

📐 Gravitational Acceleration (g)
  • Symbol: g
  • Standard value: 9.8 m/s² (approx. 10 m/s²)
  • Formula: g = GMₑ / Rₑ²
  • Does NOT depend on mass of the falling object
  • Depends on: mass of Earth & distance from centre
Earth
9.8 m/s²
Moon
1/6 of Earth
Centre of Earth
0
📉 Change in Value of g

The value of g is NOT constant — it varies with position on/in Earth.

Location g Value Reason
Poles Maximum Closer to Earth's centre (Earth is oblate)
Equator Minimum Farthest from Earth's centre + rotation effect
Going Up (altitude) Decreases Distance from centre increases
Going Down (depth) Decreases Effective mass of Earth reduces
Centre of Earth Zero (0) Equal pull from all directions
Moon's Surface 1/6 of Earth Moon has less mass & radius
⚠️ Exam Trap — Poles vs Equator
  • g is maximum at poles — frequently asked!
  • g is minimum at equator
  • Weight of a body at poles > weight at equator (because W = mg)
  • At centre of Earth, g = 0, so Weight = 0 but Mass ≠ 0
📘 Key Trick

g ∝ 1/r² → As distance from centre increases (going up), g decreases.


At depth d: g decreases linearly.


Moon: g_moon = g_earth / 6 → Weight on Moon = 1/6 of Earth weight

🪐 Kepler's Laws of Planetary Motion

Johannes Kepler gave 3 laws describing how planets orbit the Sun.

Law 1
Law of Orbits

Every planet moves in an elliptical orbit around the Sun, with the Sun at one of the two foci of the ellipse.

Law 2
Law of Areal Speed (Equal Areas)

The imaginary line joining the planet to the Sun sweeps equal areas in equal time intervals. → Planet moves faster when closer to the Sun (perihelion) and slower when farther (aphelion).

Law 3
Law of Period of Revolution (Harmonic Law)

The square of the orbital period (T²) of a planet is proportional to the cube of the semi-major axis (a³) of its orbit.

T² ∝ a³Kepler's Third Law Formula
⚠️ Exam Trap — Kepler's Laws
🛰️ Satellites
📘 Definition

Bodies revolving around a planet are called satellites. Moon is a natural satellite of Earth. INSAT, GPS etc. are artificial satellites.

  • Orbital Velocity (nearest to Earth's surface): Vₒ = √(gR)
  • Value: 8 km/s (approx.)
  • A satellite in orbit is in a state of free fall
  • Satellite feels weightlessness (apparent weight = 0)
🌐 Geostationary Satellite
Time Period
24 Hours
Height from Surface
36,000 km
Direction
West → East
  • Appears stationary relative to Earth's surface
  • Period = Earth's rotation period = 24 hours
  • Height = 36,000 km above Earth's surface
  • Rotates in the equatorial plane
  • Used for: TV broadcast, weather monitoring, communication
  • Examples: INSAT series (India)
⚠️ Exam Trap — Geostationary vs Polar
  • Geostationary → 36,000 km height, 24 hr period, equatorial orbit
  • Polar satellite → Low orbit (~500–800 km), passes over poles, used for spy/remote sensing
🚀 Escape Velocity
📘 Definition

The minimum velocity with which a body, when thrown upward from Earth's surface, can escape the gravitational field of Earth permanently (without further propulsion).

Vₑ = √(2gR)Escape Velocity Formula
11.2 km/s
Escape Vel. — Earth
2.35 km/s
Escape Vel. — Moon
√2 × Vₒ
Vₑ in terms of Vₒ
🔗 Relation: Escape Velocity vs Orbital Velocity
Vₑ = √2 × VₒEscape Velocity = √2 times Orbital Velocity
  • Orbital Velocity (Vₒ) = 8 km/s
  • Escape Velocity (Vₑ) = 11.2 km/s = √2 × 8 ≈ 11.31 km/s
  • If satellite speed increased by √2 times (~41%), it escapes Earth's gravity
  • Moon has lower escape velocity → atmosphere not retained (gases escape)
⚠️ Exam Trap
  • Escape velocity does NOT depend on mass of the object thrown
  • Escape velocity depends on mass and radius of the planet
  • If velocity < 11.2 km/s → object falls back to Earth
  • If velocity = 11.2 km/s → object just escapes Earth
  • If velocity > 11.2 km/s → object leaves with kinetic energy to spare
⚖️ Mass vs Weight
Property Mass Weight
Definition Intrinsic/inherent property of a body (amount of matter) Force of attraction on object towards Earth's centre
Symbol m W
Formula W = mg
Unit kg (kilogram) Newton (N)
Type Scalar Vector
Changes? Never changes Changes with g (location)
At Earth's centre Same Zero (g=0)
On Moon Same 1/6 of Earth weight
W = m × gWeight Formula — W in Newtons, m in kg, g in m/s²
⚠️ Exam Trap — Mass vs Weight
  • Mass is same everywhere; Weight changes with location
  • In space (far from all bodies), weight = 0 but mass ≠ 0
  • "Weightlessness" means apparent weight is zero — NOT that mass is zero
  • A spring balance measures Weight; a beam balance measures Mass
🎯 High-Frequency BPSC/BSSC Exam Points
  • Value of G = 6.67 × 10⁻¹¹ Nm²/kg² — discovered by Cavendish (1798)
  • Value of g = 9.8 m/s² (use 10 m/s² for calculations)
  • g is maximum at poles, minimum at equator
  • g = 0 at centre of Earth
  • g on Moon = 1/6 of Earth's g
  • Escape velocity of Earth = 11.2 km/s
  • Escape velocity of Moon = 2.35 km/s
  • Orbital velocity = 8 km/s
  • Vₑ = √2 × Vₒ
  • Geostationary satellite → height = 36,000 km, period = 24 hours
  • Kepler's Law 1 = Ellipse, Law 2 = Equal Areas, Law 3 = T² ∝ a³
  • Weight = 0 at centre of Earth (g=0), but Mass remains same
🔢 Important Values Quick Table
Quantity Value
G 6.67 × 10⁻¹¹ Nm²/kg²
g (Earth) 9.8 m/s²
g (Moon) ~1.63 m/s² (1/6 of Earth)
g (Centre) 0
Orbital Velocity 8 km/s
Escape Vel. Earth 11.2 km/s
Escape Vel. Moon 2.35 km/s
Geostationary Ht. 36,000 km
Geostationary Period 24 hours
📝 Formula Summary
F = G(m₁m₂)/r²Newton's Gravitational Law
g = GMₑ/Rₑ²Gravitational Acceleration
W = mgWeight
T² ∝ a³Kepler's 3rd Law
Vₒ = √(gR)Orbital Velocity
Vₑ = √(2gR) = √2 × VₒEscape Velocity
⚠️ Most Common Exam Traps
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