Calculating Proper Acceleration at Bottom of a Half Light-Year Rocket

In summary, the proper acceleration at the bottom of a half light-year tall rocket accelerating at 1g would be 2.06G. This can be calculated by considering the Rindler horizon, which is the distance at which an observer with an acceleration A would see the horizon at a distance of c^2/A behind them. Since 1g acceleration is equal to 1.03 light-years/year^2, the Rindler horizon would be 0.97 light-years behind the observer at the top of the rocket. Therefore, the bottom of the rocket would be at a distance of 0.47 light-years from the Rindler horizon, resulting in a proper acceleration of 1/A = 0.47
  • #1
idcavili
1
0
Suppose that you are at the top of a (rigid) rocket which is half a light
year tall. If the rocket is accelerating such that your proper acceleration
is 1g,

What is the proper acceleration at the bottom of the rocket?

B =
F c2
c2  F
:

This is one of the equations given:

alpha B = (alpha f c^2)/(c^2 - delta alpha f)

It seems that delta alpha f is the difference in accelerations. I can't find any equation that uses the distance. Is it OK to use the distance in this one?
 
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  • #2
Well, you could make use of the fact that any object undergoing Born rigid acceleration (such that each point has constant proper acceleration, and the length of the object in the instantaneous inertial rest frame of any point on the object doesn't change from one moment to the next) must be at rest in a Rindler coordinate system. An observer with an acceleration A has the Rindler horizon at a distance of c2/A behind them according to the article, and 1G acceleration works out to 1.03 light-years/year2, so the Rindler horizon would be 1/1.03 = 0.97 light-years behind the observer at the top of the rocket, which means it's OK for the rocket to be 0.5 light-years long. In this case the bottom would be at a distance of 0.97-0.5 = 0.47 light-years from the Rindler horizon, which means it should have a proper acceleration of 1/A = 0.47, meaning A = 1/0.47 = 2.12 light-years/year2, or about 2.12/1.03 = 2.06G.

edit: is this a homework problem? If so I guess you'd have to use an equation that was actually discussed in the chapter in which the problem appeared...what are the meanings of the various symbols in the equation you posted?
 
Last edited:

FAQ: Calculating Proper Acceleration at Bottom of a Half Light-Year Rocket

How is proper acceleration defined in the context of a half light-year rocket?

In the context of a half light-year rocket, proper acceleration refers to the rate of change of an object's velocity with respect to its own proper time. It is a measure of the acceleration experienced by an object as an observer moving along with it would perceive it.

How do you calculate proper acceleration at the bottom of a half light-year rocket?

To calculate proper acceleration at the bottom of a half light-year rocket, you would use the formula a = γ^3 * g, where a is the proper acceleration, γ is the Lorentz factor (calculated using the velocity of the rocket and the speed of light), and g is the acceleration due to gravity.

What units are proper acceleration measured in?

Proper acceleration is typically measured in units of meters per second squared (m/s^2). However, in the context of relativistic physics, it can also be measured in units of g-forces (multiples of the acceleration due to gravity on Earth).

How does proper acceleration change as the rocket approaches the speed of light?

As the rocket approaches the speed of light, the Lorentz factor γ increases, causing the proper acceleration to increase as well. However, due to the inverse relationship between proper acceleration and proper time, the perceived acceleration by an observer on the rocket will decrease as the speed of light is approached.

What other factors can affect proper acceleration in a half light-year rocket?

Aside from the velocity and acceleration due to gravity, other factors that can affect proper acceleration in a half light-year rocket include the mass of the rocket and any external forces acting on it, such as air resistance or gravitational pulls from other celestial bodies.

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