Calculating Fuel Efficiency of Rocket Going Near c

In summary, calculating the fuel efficiency of a rocket travelling near the speed of light would involve calculating the change in energy of the rocket, dividing that by the change in energy of the fuel, and then using the relativistic rocket equation to find the exhaust velocity.
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Peter564
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How would you calculate the fuel efficiency of a rocket (around 10 tonnes) going near the speed of light?
 
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Peter564 said:
How would you calculate the fuel efficiency of a rocket (around 10 tonnes) going near the speed of light?
You would take the change in energy of the rocket and divide it by the change in energy of the fuel.
 
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Peter564 said:
How would you calculate the fuel efficiency of a rocket (around 10 tonnes) going near the speed of light?

There are several things you might be interested in - are you interested in how much fuel you need to get a specified increase in velocity?

Basically, you need the relativistic rocket equation, and the exhaust velocity of the rocket, if that's what you're trying to measure. I would suggest https://math.ucr.edu/home/baez/physics/Relativity/SR/Rocket/rocket.html for the relativistic rocket equation. Wikipedia also has an entry which I'm less familiar with, https://en.wikipedia.org/wiki/Relativistic_rocket.

Other interesting cases you might consider are a relativistic laser driven light sail with perfect transmission efficiency. But I don't recall seeing anything written about that, though it's an interesting case to analyze. Doppler shift of the light from the laser makes the acceleration of the rocket taper off as it reaches higher and higher velocities.

It's really up to you to give more details of what you consider to be "fuel efficiency", one suggestion is the amount of energy in the burned fuel vs the amount of energy that the rocket gains in some specific frame of reference where the rocket's velocity is given by some particular value. You will, of course, find in this case that choosing this definition of "fuel efficiency" makes the "fuel efficiency" dependent on the choice of frame of reference in which it's mentioned.

The key parameters I see are the exhaust velocity of the rocket, the starting mass ratio of the rocket, and the current velocity of the rocket.
 

What is the formula for calculating fuel efficiency of a rocket going near c?

The formula for calculating fuel efficiency of a rocket going near c is: fuel efficiency = (change in kinetic energy) / (change in mass of fuel).

What is the speed of light and why is it important in calculating fuel efficiency?

The speed of light, denoted by the letter c, is a fundamental constant in physics that represents the maximum speed at which all matter and information can travel. It is important in calculating fuel efficiency because it is the theoretical limit for how fast a rocket can travel and therefore affects the amount of fuel needed to reach near c.

How is the mass of fuel calculated in the fuel efficiency formula?

The mass of fuel is calculated by subtracting the final mass of the rocket from the initial mass of the rocket. This difference represents the amount of fuel used during the rocket's acceleration.

What units are used for calculating fuel efficiency?

The units used for calculating fuel efficiency depend on the units used for the change in kinetic energy and change in mass of fuel. For example, if the change in kinetic energy is measured in joules and the change in mass of fuel is measured in kilograms, then the fuel efficiency would be measured in joules per kilogram (J/kg).

Can fuel efficiency be greater than 1?

Yes, fuel efficiency can be greater than 1. This would occur if the change in kinetic energy is greater than the change in mass of fuel, meaning that the rocket is able to accelerate using less fuel than expected. However, this is not possible for a rocket going near c as it would require infinite energy.

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