How Does a Relativistic Photon Rocket Calculate Acceleration and Speed?

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SUMMARY

The discussion focuses on the calculations involved in determining the acceleration and speed of a relativistic photon rocket. Key equations include the 4-vector acceleration formula and the relationship between proper acceleration and relativistic effects, specifically showing that \( a = \frac{a_0}{\gamma^3} \). The proper acceleration is derived from the mass-energy equivalence principle, leading to \( a_0(\tau) = \alpha c e^{-\alpha \tau} \). Additionally, the discussion highlights the impact of Doppler shift on photon energy as perceived from different frames of reference.

PREREQUISITES
  • Understanding of special relativity concepts, particularly Lorentz transformations
  • Familiarity with 4-vector notation and relativistic dynamics
  • Knowledge of mass-energy equivalence and its implications in relativistic physics
  • Basic calculus for solving differential equations related to motion
NEXT STEPS
  • Study the derivation of Lorentz transformations in special relativity
  • Learn about the implications of relativistic mass and energy in particle physics
  • Explore the concept of Doppler effect in the context of relativistic speeds
  • Investigate advanced topics in relativistic rocket dynamics and propulsion systems
USEFUL FOR

Students of physics, aerospace engineers, and anyone interested in the principles of relativistic motion and photon propulsion technologies.

unscientific
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Homework Statement


(a) Show ##a = \frac{a_0}{\gamma^3}##.
(b) Find proper acceleration of rocket
(c) Find speed as a function of time.
(d) Find acceleration of second rocket.

2011_B1_Q5.png

Homework Equations

The Attempt at a Solution


Part(a)
4-vector acceleration is given by ##\gamma^2 \left[ \frac{\gamma^2}{c}(\vec u \cdot \vec a), \frac{\gamma^2}{c^2}(\vec u \cdot \vec a)\vec u + \vec a \right]##.
For acceleration parallel to velocity, using invariance we have ##a_0^2 = a^2\gamma^6##. Thus we show that
a = \frac{a_0}{\gamma^3}

Part(b)
We know that ##\frac{M(\tau)}{d\tau} = -\alpha M(\tau)##, so solving we have ##M(\tau) = M_0 e^{-\alpha \tau}##. Considering the change in energy of the photon in time ##d\tau##, we have ##\frac{dE}{d\tau} = c \frac{dp}{d\tau} = cm_0 a_0##. Also in time ##d\tau##, the change in mass converted to energy is ##dE=c^2dM = -\alpha M_0 e^{-\alpha \tau} c^2 d\tau##. Thus we have the acceleration as
a_0 (\tau) = \alpha c e^{-\alpha \tau}

Part(c)
I'm not sure how to do this part. I have ##v = c \tanh \left( \frac{a_0 \tau}{c} \right)##.

Part(d)
Same concept as part(b). In time ##dt##, energy of photons produced is ##\alpha M_0 c^2 dt = p c##. Thus upon reflection, the change in momentum in time ##dt## is ##\Delta p = 2\alpha m_0 c dt##. Acceleration is ##a = 2\alpha c##. Finally, we have ##a_0 = \gamma^3 a##:
a_0 = \gamma^3 (2 \alpha c) = \frac{2\alpha a}{\left( 1 - \frac{v^2}{c^2} \right)^{-\frac{3}{2}}}

How do I do part (c)?
 
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unscientific said:
Part(b)
We know that ##\frac{M(\tau)}{d\tau} = -\alpha M(\tau)##, so solving we have ##M(\tau) = M_0 e^{-\alpha \tau}##. Considering the change in energy of the photon in time ##d\tau##, we have ##\frac{dE}{d\tau} = c \frac{dp}{d\tau} = cm_0 a_0##.

In the right hand side of the last equation, shouldn't ##m_0## be replaced by ##M(\tau)##?

Part(d)
Same concept as part(b). In time ##dt##, energy of photons produced is ##\alpha M_0 c^2 dt = p c##. Thus upon reflection, the change in momentum in time ##dt## is ##\Delta p = 2\alpha m_0 c dt##.

Due to the motion of the rocket relative to the launch pad, the rate at which photons arrive at the rocket according to launch-pad time is not the same as the rate at which photons are produced according to lauch-pad time. Also in the launch-pad frame, there is a doppler shift in the frequency (or energy) of the photons as they reflect off of the moving rocket.
 
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