How does special relativity apply to the rocket equation?

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SUMMARY

The discussion centers on the application of special relativity (SR) to the Tsiolkovsky rocket equation, specifically addressing misconceptions about SR's applicability to non-inertial frames. Participants clarify that SR is valid in flat spacetime, which allows for the derivation of the relativistic rocket equation even under acceleration. The hyperbolic motion equation, which relates proper and dilated time, is also discussed, with references to the mathematical foundations necessary for understanding these concepts. Key resources, including John Baez's article and Taylor & Wheeler's "Spacetime Physics," are recommended for further study.

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  • Understanding of special relativity principles
  • Familiarity with the Tsiolkovsky rocket equation
  • Basic knowledge of hyperbolic functions
  • Mathematical skills including calculus for non-inertial frames
NEXT STEPS
  • Study the derivation of the relativistic rocket equation using conservation of momentum
  • Learn about hyperbolic motion equations and their applications in spacetime
  • Explore the concept of four-velocity and four-acceleration in special relativity
  • Read Taylor & Wheeler's "Spacetime Physics" for a comprehensive introduction to special relativity
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Students of physics, particularly those interested in astrodynamics and special relativity, as well as educators seeking to enhance their understanding of the relativistic rocket equation.

  • #31
Here is my try. There are two ways. One is to use coordinate time and the other is to work with the manifestly covariant equations of motion. For the latter way we use the normalized four-velocity and assume that the constant acceleration is in ##x^1##-direction. So we can work in (1+1)-dimensional Minkowski space.

The normalized four-velocity then reads
$$(u^{\mu})=\begin{pmatrix} \cosh y \\ \sinh y \end{pmatrix},$$
where ##y## is the (momentum-space) rapidity, which parametrization works in the constraint ##u_{\mu} u^{\mu}=1##.

The equations of motion are
$$\mathrm{d}_{\tau} u^0=\alpha/c u^1, \quad \mathrm{d}_{\tau} u^1=c \alpha/c u^0.$$
The two equations are not independent because of the constraint. So we use the 2nd equation with the parametrization using the rapidity,
$$\cosh y \mathrm{d}_{\tau} y =\alpha/c \cosh y \; \Rightarrow \; y=\frac{\alpha \tau}{c}+y_0.$$
A direct check shows that indeed also the first eom is fulfilled so we have
$$(u^{\mu})=\begin{pmatrix} \cosh(\alpha \tau/c+y_0) \\ \sinh(\alpha \tau/c+y_0) \end{pmatrix}.$$
The spacetime vector is then defined by
$$\mathrm{d}_{\tau} x^{\mu}=c u^{\mu}$$
from which
$$x^{\mu}=\begin{pmatrix} \frac{c^2}{\alpha} \sinh(\alpha \tau/c+y_0) \\ x_0^{1} + \frac{c^2}{\alpha} [\cosh(\alpha \tau/c + y_0)-1]. \end{pmatrix}$$
I've chosen the initial time such that ##t_0=t(0)=0##.

In terms of coordinate time we have
$$x^1(t)=x_0^1 + \frac{c^2}{\alpha} \left [\sqrt{\alpha^2 t^2/c^2+1}-1 \right]$$
and for the velocity
$$v(t)=\mathrm{d}_t x^1=\frac{\alpha t}{\sqrt{\alpha^2 t^2/c^2+1}}.$$
 
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