Gravitation
Overview: This chapter explores the fundamental force of gravity, planetary motion, and satellite mechanics.
1. Kepler's Laws of Planetary Motion
- Law of Orbits (1st): All planets move in elliptical orbits with the Sun at one of the foci.
- Law of Areas (2nd): The line joining the planet to the Sun sweeps out equal areas in equal intervals of time. (dA/dt = constant = L/2m). consequence of conservation of angular momentum.
- Law of Periods (3rd): The square of time period is proportional to the cube of semi-major axis.
T² ∝ a³
2. Universal Law of Gravitation
Every particle attracts every other particle with a force proportional to product of masses and inversely proportional to square of distance.
F = G (m1m2) / r²
G = 6.67 × 10-11 N m²/kg²
3. Acceleration due to Gravity (g)
On surface of Earth: g = GM / R² ≈ 9.8 m/s².
Variation of g
- At Altitude h: gh = g (1 - 2h/R) [for h << R]
- At Depth d: gd = g (1 - d/R)
g is maximum at surface/poles, minimum at equator (due to rotation).
4. Gravitational Potential Energy (U)
Energy possessed by a body due to its position in gravitational field. Zero at infinity.
U = - (GMm) / r
Gravitational Potential (V)
Potential energy per unit mass.
V = - GM / r
5. Orbital & Escape Velocity
Escape Velocity (ve)
Minimum speed required to escape Earth's gravity field.
ve = √(2GM/R) = √(2gR) ≈ 11.2 km/s
Orbital Velocity (vo)
Velocity required to keep a satellite in orbit close to Earth.
vo = √(GM/R) = √(gR) ≈ 7.9 km/s
Relation: ve = √2 vo
Energy of Satellite
Kinetic K = GMm/2r. Potential U = -GMm/r. Total E = -GMm/2r.
Numericals
Force Calc
Q1. Two spheres of mass 50kg and 10kg are 2m apart. Find grav-force.
(G=6.67x10-11)
F = G m1 m2 / r2
F = 6.67×10-11 × 50 × 10 / 22
F = 6.67×10-11 × 500 / 4
F = 6.67 × 125 × 10-11
F = 8.3 × 10-9 N
Variation of g
Q2. At what height above Earth's surface does 'g' become half its surface value?
(R=6400km)
gh = g / 2
gh = g R2 / (R+h)2
1/2 = R2 / (R+h)2
√2 = (R+h)/R
1.414 R = R + h
h = 0.414 R
h = 2650 km
Orbital Velocity
Q3. Calculate orbital velocity of a satellite near Earth's surface. (g=9.8,
R=6.4x106)
vo = √(gR)
vo = √(9.8 × 6.4 × 106)
vo = √(62.72 × 106)
vo ≈ 7.9 × 103 m/s
vo = 7.9 km/s
Gravitational Potential Energy
Q4. Calculate potential energy of a 100kg object at Earth's surface.
(M=6x1024kg, R=6.4x106m)
U = - GMm / R
U = - (6.67×10-11 × 6×1024 × 100) /
6.4×106
U = - (40 × 1015) / 6.4×106
U = - 6.25 × 109 J
Negative sign indicates binding.
Depth Calculation
Q5. Find depth d where g is 75% of surface value.
gd = 0.75 g
gd = g(1 - d/R)
0.75 = 1 - d/R
d/R = 0.25
d = R/4 = 1600 km
Escape Velocity
Q6. If a planet has mass 4 times Earth and same radius, find escape velocity.
(vearth = 11.2)
ve = √(2GM/R)
v is proportional to √M
v' / v = √(M'/M)
v' / 11.2 = √(4M/M) = 2
v' = 22.4 km/s
Kepler's T-Squared Law
Q7. A satellite orbits at height R above surface (radius 2R). Geo-stationary orbits at
6R (radius 7R). T for first?
T2 = 24 hrs, r2 = 7R, r1 = 2R
(T1/T2)2 = (r1/r2)3
T1 = T2 × (2/7)3/2
T1 = 24 × √(8/343)
T1 ≈ 24 × 0.15
T1 ≈ 3.6 hours
Weightlessness
Q8. What should be Earth's angular speed so value of g at equator becomes zero?
g' = g - Rω2 = 0
ω = √(g/R)
ω = √(9.8 / 6.4×106)
ω = 1.24 × 10-3 rad/s
Energy to Orbit
Q9. Energy required to lift 500kg mass to orbit radius 4R (h=3R)?
Total Energy Change (Potential + Kinetic needed to orbit)
Actually Q asks work to lift or launch? Let's assume lift to height h.
ΔU = Uf - Ui
ΔU = -GMm/4R - (-GMm/R)
ΔU = (3/4) GMm/R = (3/4) mgR
Work = 0.75 × 500 × 10 × 6.4×106
Work = 2.4 × 1010 J
Force Ratio
Q10. Two particles of equal mass move in a circle under mutual gravitation. Speed?
Grav force = Centripetal force
Gmm/(2R)2 = mv2/R
Gm2/4R2 = mv2/R
v2 = Gm/4R
v = √(Gm/4R)
Equations & Formulas
| Concept | Formula |
|---|---|
| Grav Force | F = G m1 m2 / r² |
| Acc due to Gravity | g = GM / R² |
| g at Height h | gh = g (1 - 2h/R) |
| g at Depth d | gd = g (1 - d/R) |
| Grav Potential | V = - GM / r |
| Potential Energy | U = - GMm / r |
| Orbital Velocity | vo = √(GM/r) |
| Escape Velocity | ve = √(2GM/R) |
| Time Period | T² = (4π²/GM) r³ |
| Total Satellite Energy | E = - GMm / 2r |
50 NEET Facts
Key points for Gravitation.
1. Weakest Force
Gravitational force is the weakest of the four fundamental forces in nature.
2. Central Force
Acts along the line joining the centers of two masses. It is a conservative force.
3. Medium Independence
Gravitational force does not depend on the intervening medium between masses.
4. Mass vs Weight
Mass is constant everywhere. Weight (W=mg) varies with g. Weight is zero at Earth's center.
5. Inertial vs Gravitational Mass
They are experimentally found to be equal (Equivalence Principle).
6. Value of G
Universal Gravitational Constant G = 6.67 x 10-11 Nm²/kg². First measured by Cavendish.
7. g Max/Min
g is max at Poles (R is min) and min at Equator (R is max).
8. Effect of Rotation
Rotation of Earth reduces g at equator by Rω². No effect at poles.
9. g at Infinity
Value of g becomes zero at infinite distance.
10. Gravitational Shielding
Impossible. You cannot shield a body from gravity.
11. Kepler's 1st Law
Orbits are elliptical. Sun is at one focus, not the center.
12. Kepler's 2nd Law
Areal velocity is constant. Implies conservation of angular momentum (L = constant).
13. Orbital Speed Variation
Planets move faster when closer to Sun (Perihelion) and slower when far (Aphelion).
14. Escape Velocity Value
Independent of mass of the body projected. Depends only on Mass and Radius of planet.
15. Escape Velocity Angle
Does not depend on angle of projection.
16. Atmosphere
Moon has no atmosphere because vrms of gas molecules > vescape.
17. Geostationary Satellite
T = 24 hours. Height = 36,000 km. Orbits in equatorial plane. West to East.
18. Polar Satellite
Low altitude (500-800 km). T approx 100 min. Scans entire Earth strip by strip.
19. Binding Energy
Energy required to remove satellite to infinity. BE = +GMm/2r.
20. Negative Potential
Potential is negative because work is done by the field (attractive forces) to bring mass from infinity.
21. Shell Theorem 1
Gravitational field inside a uniform spherical shell is Zero.
22. Shell Theorem 2
Outside spatial shell, it behaves as if entire mass is at center.
23. Weightlessness
In a satellite, normal reaction is zero because grav force provides centripetal force entirely.
24. Black Hole
Body so dense that Escape Velocity > Speed of Light (c).
25. Potential inside Earth
Potential decreases from surface to center. Center is not zero potential; it is -3GM/2R.
26. g depth vs height
Decrease in g at depth d is equal to decrease at height h=d/2 (for small h). g decreases faster going up.
27. Two Star System
Both stars revolve around their common Center of Mass with same angular velocity ω.
28. Tidal Waves
Caused by gravitational pull of Moon (and Sun) on Earth's oceans.
29. Intensity of Field
E = F/m. Dimension is of acceleration [LT-2].
30. Work around closed path
Work done by gravity in a round trip is Zero (Conservative force).
31. Parking Orbit
Another name for Geostationary orbit. Satellite appears fixed (parked).
32. Communication Satellites
Usually geostationary to maintain constant link with ground antennas.
33. Remote Sensing
Uses Polar satellites (low orbit, high resolution).
34. Gravitational Mass
Determined by weighing. W = mg.
35. Inverse Square Law
If force depended on 1/r (instead of r²), closed stable orbits would not exist.
36. Speed of Gravity
In General Relativity, changes in gravity propagate at speed of light (Gravitational Waves).
37. Equipotential Surfaces
For a point mass, they are spherical shells.
38. Air Resistance
Satellites in low orbit eventually spiral down due to air drag, losing energy (actually speed increases as r
decreases, paradox).
39. Relation ve vs vo
Escape velocity is 41.4% higher than orbital velocity (close to surface).
40. Time Period at Surface
A satellite skimming Earth surface would have T approx 84.6 minutes.
41. Zero Gravity
Exists at the center of Earth. Or far in deep space (technically approaches zero).
42. Sphere of Influence
Region around a planet where its gravity dominates over Sun.
43. Retrograde Orbit
Orbit opposite to Earth's rotation (East to West). Harder to launch.
44. Launch Velocity
Rockets are launched Eastward to gain from Earth's rotation speed.
45. Multi-stage Rocket
Used to reduce mass of carrier as fuel burns, allowing higher final velocity.
46. Fall through Earth Tunnel
If you drop a stone in a tunnel through Earth center, it executes SHM. T = 84.6 min.
47. Inertial Frame
Earth is not strictly inertial due to rotation and revolution.
48. Sun's Mass
Calculated using Earth's orbital period and radius (Kepler's 3rd Law).
49. Spring Balance Reading
Varies with latitude. Max at poles, min at equator.
50. Beam Balance
Measures mass. Reading is constant everywhere regardless of g.
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