JEE Main · Physics ↓ Falling

Gravitation appeared 22 times across 3 years — 2.5% of Physics. This question is from Escape Velocity.

Year 2026 2025 2024 Total
Questions 5 9 8 22

An object is kept at rest at a distance of 3R above the earth's surface where R is earth's radius. The minimum speed with which it must be projected so that it does not return to earth is: (Assume M= mass of earth, G= Universal gravitational constant)

Solution & Explanation

Related Formula

Conservation of Total Mechanical Energy: Eᵢ = Ef

Uᵢ + Kᵢ = Uf + Kf
Core Logic

The initial distance from the center of the earth is r = R + 3R = 4R. Initial mechanical energy:

Eᵢ = -(GMm)/(4R) + (1)/(2)mv²

To just escape to infinity, the final mechanical energy at infinity must be at least zero: Ef = 0

Step 1: Apply Energy Conservation

Setting initial energy equal to zero:

-(GMm)/(4R) + (1)/(2)mv² = 0

(1)/(2)v² = (GM)/(4R) v = √((GM)/(2R))

Escape projection trajectory from height 3R
Escape projection trajectory from height 3R

Pattern Recognition

Be extremely careful with the phrase 'above the earth's surface'. Distance from center r = R + h. Escape condition always sets net mechanical energy ≥ 0.

Chapter Mix

Class 11 Physics: Gravitation

Reference Study Guides

More Gravitation Previous-Year Questions

Q44 jee_main_2026_21_jan_morning Satellite Energy
Initially a satellite of 100 kg is in a circular orbit of radius 1.5RE. This satellite can be moved to a circular orbit of radius 3RE by supplying α × 10⁶J of energy. The value of α is ____. (Take Radius of Earth RE = 6 × 10⁶ m and g = 10 m/s²)
  • A. 150
  • B. 500
  • C. 100
  • D. 1000

Solution

Related Formula
E = (-GME m)/(2r) Δ E = Ef - Eᵢ g = (GME)/(RE²) GME = g RE²
Core Logic

Energy of a satellite in a circular orbit is given as E = (-GME m)/(2r) where r is the radius of the circular orbit. Required energy to be supplied Δ E = Ef - Eᵢ:

Δ E = ( (-GME m)/(2(3RE)) ) - ( (-GME m)/(2(1.5RE)) ) Δ E = (-GME m)/(6RE) + (GME m)/(3RE) = (GME m)/(6RE)
Step 1: Evaluate Delta E

Substitute GME = g RE² into the expression:

Δ E = ((g RE²) m)/(6RE) = (1)/(6) m g RE = (1)/(6) × 100 × 10 × (6 × 10⁶) = 1000 × 10⁶ J

Comparing with α × 10⁶ J, we get α = 1000.

Pattern Recognition

Orbital transition energy is always Δ E = (GMm)/(2) ((1)/(rᵢ) - (1)/(rf)). Never forget the factor of 2 in the denominator (which accounts for kinetic energy contribution in orbit).

Chapter Mix

Class 11 Physics: Gravitation

Q30 jee_main_2026_22_january_morning Escape Velocity
The escape velocity from a spherical planet A is 10 km/s. The escape velocity from another planet B whose density and radius are 10% of those of planet A, is \_\_\_\_ m/s.
  • A. 1000
  • B. 200√(5)
  • C. 100√(10)
  • D. 1000√(2)

Solution

Related Formula
Vₑ = √((2GM)/(R)) = √((2G ρ (4π R³)/(3))/(R)) Vₑ ∝ √(ρ) × R
Core Logic

Given density and radius of B are 10% (0.1) of planet A:

((Vₑ)B)/((Vₑ)A) = √((ρB)/(ρA)) × (RB)/(RA) = √(0.1) × 0.1 = 110√(10) (Vₑ)B = 10 × 100010√(10) = 100√(10) m/sec
Pattern Recognition

Sees: Escape velocity scaling with density and radius. Shortcut: Express escape velocity in terms of density ρ and radius R, then take ratios. Check: Matches option (3). ✓

Chapter Mix

Class 11 Physics: Gravitation

Q35 jee_main_2026_22_january_morning Gravitational Force and Superposition
Net gravitational force at the centre of a square is found to be F₁ when four particles having mass M, 2M, 3M and 4M are placed at the four corners of the square as shown in figure and it is F₂ when the positions of 3M and 4M are interchanged. The ratio F₁F₂ is α√(5). The value of α is \_\_\_\_.
Gravitation diagram for Q35 - JEE Main 2026 January Morning
Four point masses placed at the corners of a square.
  • A. 2
  • B. 3
  • C. 1
  • D. 2√(5)

Solution

Related Formula
F = (G m₁ m₂)/(r²)
Core Logic

Solution diagram for Q35 - JEE Main 2026 Morning
Four point masses placed at the corners of a square.

Initial configuration:

F₁ = 2√(2) (Gmm₀)/(r²)$|

New configuration (after interchanging 3M and 4M):

F_2 = \sqrt{10} \frac{Gmm_0}{r^2}Ratio:\frac{F_1}{F_2} = \frac{2\sqrt{2}}{\sqrt{10}} = \frac{2}{\sqrt{5}} \implies \alpha = 2$$
Pattern Recognition

Sees: Gravitational force vector sum at center of square. Shortcut: Compute net vector resultants for both mass configurations and take ratio. Check: Matches option (1). ✓

Chapter Mix

Class 11 Physics: Gravitation

Q39 jee_main_2026_22_january_evening Satellite Motion and Time Period
Given below are two statements : Statement I : A satellite is moving around earth in the orbit very close to the earth surface. The time period of revolution of satellite depends upon the density of earth. Statement II: The time period of revolution of the satellite is T = 2π Rₑg (for satellite very close to the earth surface), where Rₑ radius of earth and g acceleration due to gravity. In the light of the above statements, choose the correct answer from the options given below :
  • A. Both Statement I and Statement II are false
  • B. Both Statement I and Statement II are true
  • C. Statement I is true but Statement II is false
  • D. Statement I is false but Statement II is true

Solution

Related Formula
T = 2π √((R³)/(GM)) M = ρ · (4)/(3)π R³ g = (GM)/(R²)
Core Logic

Evaluating Statement I: Substituting total mass M = ρ · (4)/(3)π R³ into time period formula:

T = 2π √((R³)/(G (ρ · (4)/(3)π R³))) = √((3π)/(G ρ))

Hence, time period depends inversely on the square root of Earth's density ρ. Statement I is true.

Evaluating Statement II: Substituting g = (GM)/(Rₑ²) into T = 2π √((Rₑ³)/(GM)):

T = 2π √((Rₑ)/(g))

Statement II is also true.

Step 1: Final Conclusion

Both Statement I and Statement II are true.

Pattern Recognition

Near-surface satellite shortcut: T = √(3π / (Gρ)) ≈ 84.6 min. Shows direct dependence on Earth's density ρ and formula T = 2π √(Rₑ / g).

Chapter Mix

Class 11 Physics: Gravitation

Q45 jee_main_2026_24_january_morning Gravitational Potential Energy
Three masses 200 kg, 300 kg and 400 kg are placed at the vertices of an equilateral triangle with sides 20 m. They are rearranged on the vertices of a bigger triangle of side 25 m and with the same centre. The work done in this process ____ J. (Gravitational constant G = 6.7 × 10⁻¹¹ N m² / kg²)
  • A. 9.86 × 10⁻⁶
  • B. 2.85 × 10⁻⁷
  • C. 1.74 × 10⁻⁷
  • D. 4.77 × 10⁻⁷

Solution

Related Formula
U = -(Gm₁ m₂)/(r) Wₑₓₜ = Δ U = Uf - Uᵢ
Core Logic

Equilateral triangle mass configuration scaling
Equilateral triangle mass configuration scaling

Initial potential energy of the system (rᵢ = 20 m):

Uᵢ = -(G)/(rᵢ) (m₁ m₂ + m₂ m₃ + m₁ m₃) Uᵢ = -6.67 × 10⁻¹¹20 [200 × 300 + 300 × 400 + 200 × 400] Uᵢ = -6.67 × 10⁻¹¹20 [60000 + 120000 + 80000] Uᵢ = -6.67 × 10⁻¹¹20 × 260000 = -86.71 × 10⁻⁸ J

Equilateral triangle mass configuration scaling
Equilateral triangle mass configuration scaling

Final potential energy of the system (rf = 25 m):

Uf = -(G)/(rf) (260000) Uf = -6.67 × 10⁻¹¹25 × 260000 Uf = -69.36 × 10⁻⁸ J
Step 1: Calculate Work Done

The work done by an external agent is equal to the change in potential energy:

Δ U = Uf - Uᵢ Δ U = (-69.36 × 10⁻⁸) - (-86.71 × 10⁻⁸) Δ U = (86.71 - 69.36) × 10⁻⁸ = 17.35 × 10⁻⁸ J ≈ 1.74 × 10⁻⁷ J
Pattern Recognition

When an entire geometric configuration is isotropically scaled (e.g., side a to b), the total potential energy scales by the ratio of their reciprocals. Uf = Uᵢ (rᵢ/rf).

Chapter Mix

Class 11 Physics: Gravitation Class 11 Physics: Work, Energy and Power

More Gravitation Questions — jee_main_2025_04_april_evening

Practice all Gravitation previous-year questions →

Rankbit System
JEE Physics: Waves (+15.5%) | Electrostatics: Concentric Shells (-29.7%) | Modern Physics: Photoelectric Clones (+34.2%) | Mathematics: Definite Integrals (+18.1%) | Chemistry: Coordination Splitting (-11.4%) | JEE Physics: Waves (+15.5%) | Electrostatics: Concentric Shells (-29.7%) | Modern Physics: Photoelectric Clones (+34.2%) | Mathematics: Definite Integrals (+18.1%) | Chemistry: Coordination Splitting (-11.4%)