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Question #43526

Difficulty: 8/10 | 🟢 Free

The Question

A massive spacecraft is moving directly away from Earth with a constant relativistic velocity VV. Inside the spacecraft, a motorized platform is mounted on a track parallel to the direction of motion. A small light source of mass mm is attached to this platform via a spring of force constant kk. Let ω0=k/m\omega_0 = \sqrt{k/m}.

Initially (t≤0t \le 0), the platform is at rest relative to the spacecraft, and the mass is at rest in its equilibrium position.

At t=0t=0, the platform begins to oscillate along the track such that its acceleration relative to the spacecraft is ap(t)=a0cos⁡(ωt)a_p(t) = a_0 \cos(\omega t) (where the positive direction is away from Earth), with ω=ω0/2\omega = \omega_0 / 2 and a0a_0 being a positive constant.

The light source continuously emits a signal of proper frequency ν0\nu_0 towards Earth. Assume the maximum speed uu of the mass relative to the spacecraft satisfies u≪cu \ll c.

Which of the following expressions gives the maximum frequency of the signal observed on Earth during the subsequent motion?

Options

  • A.

    ν0c−Vc+V(1+23a0cω0)\nu_0 \sqrt{\frac{c-V}{c+V}} \left(1 + \frac{2\sqrt{3} a_0}{c \omega_0}\right)

  • B.

    ν0c−Vc+V(1+4a0cω0)\nu_0 \sqrt{\frac{c-V}{c+V}} \left(1 + \frac{4 a_0}{c \omega_0}\right)

  • C.

    ν0c−Vc+V(1+a0cω0)\nu_0 \sqrt{\frac{c-V}{c+V}} \left(1 + \frac{a_0}{c \omega_0}\right)

  • D.

    ν0c−Vc+V(1+8a03cω0)\nu_0 \sqrt{\frac{c-V}{c+V}} \left(1 + \frac{8 a_0}{3 c \omega_0}\right)

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Correct Answer

Step-by-Step Solution

Explanation

How the Examiner Thinks

Intuition_Breaker

Train your brain to resist "obvious" answers that are designed to deceive your intuition.

Concepts Behind This Question

Frame of Reference Dependency|Vertical Oscillations|SHM Definition via Differential Equation|Small Angle Approximation

Why This Question Is Tricky

Common Mistakes

This question tests the student's ability to synthesize non-inertial frame dynamics, forced harmonic oscillations, and the relativistic Doppler effect.

The primary trap lies in the calculation of the maximum velocity of the mass relative to the spacecraft.

Students often incorrectly assume the maximum velocity is simply the sum of the amplitudes of the individual oscillating terms (leading to Option B), or they evaluate the velocity at an incorrect phase angle like π/2\pi/2 (leading to Option D).

Furthermore, failing to account for the platform's own velocity and only using the relative velocity vrelv_{rel} will yield a completely incorrect maximum speed.

Mastery requires setting up the exact time-dependent velocity function and rigorously maximizing it using calculus before applying the first-order Doppler shift correction.

Quick Facts About This Question

Question Information

SubjectPhysics
ChapterMotion in a Straight Line - Class 11 Part 1
ConceptFrame of Reference Dependency
Difficulty8
Cognitive Load7
Target Solve Time160 sec
AccessFree