What is the difference between thrust and thrust density?

In summary, "Thrust" is a measure of the force produced by a propulsion unit, "Nozzle exit area" is a measure of how much area the nozzle uses, and "Thrust density" is a measure of how much force per unit area the propulsion unit produces.
  • #1
AdrianHudson
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0000126.001&db_key=AST&bits=4&res=100&filetype=.gif


The picture above has thrust density as a column and I am not too sure what that is. Can anyone explain to me what the difference between thrust and thrust density? Thank you for your answers!
 

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  • #2
The clue is in the table headings.
  • "Thrust" is measured in Newtons.
  • "Nozzle exit area" is measured in square metres.
  • "Thrust density" is measured in Newtons per square metre.
It shouldn't be too difficult to work it out from that.
 
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  • #3
DrGreg said:
The clue is in the table headings.
  • "Thrust" is measured in Newtons.
  • "Nozzle exit area" is measured in square metres.
  • "Thrust density" is measured in Newtons per square metre.
It shouldn't be too difficult to work it out from that.

Ahh! So its the thrust produced per m2 of the nozzle area. Therefore that means that if you had nozzle "A" that has a surface area of 0.5m2 with a thrust of 10 Newtons and Nozzle "B" that has a surface area of 1m2 with a thrust of 10Newtons. Nozzle "A" is producing more thrust density?

Am I wrong in classifying thrust density as an efficiency of the given propulsion unit?
 
  • #4
AdrianHudson said:
Ahh! So its the thrust produced per m2 of the nozzle area. Therefore that means that if you had nozzle "A" that has a surface area of 0.5m2 with a thrust of 10 Newtons and Nozzle "B" that has a surface area of 1m2 with a thrust of 10Newtons. Nozzle "A" is producing more thrust density?

Am I wrong in classifying thrust density as an efficiency of the given propulsion unit?
Not really. It has units of force per unit area or, equivalently, of energy per unit volume. But unless you are also given something like the density (mass per unit volume) of the exhaust stream, it cannot tell you the exhaust velocity.

You could, for instance, have an ion drive with an ultra high exhaust velocity (very mass-efficient and very energy-inefficient). The exhaust stream would also be very sparse and would likely have a low thrust density.
 
Last edited:
  • #5
DrGreg said:
  • "Thrust density" is measured in Newtons per square metre.

So it's pressure?

Cheers
 

1. What is thrust and thrust density?

Thrust is a force that propels an object forward by pushing against a medium, such as air or water. It is typically measured in units of newtons (N). Thrust density is the amount of thrust per unit of area, typically measured in newtons per square meter (N/m²).

2. How are thrust and thrust density related?

Thrust and thrust density are directly related, as thrust density is simply the thrust divided by the area over which it is applied. This means that as thrust increases, so does thrust density, and vice versa.

3. What is the difference in their applications?

Thrust is commonly used in the field of aerospace to measure the force produced by jet engines or rockets. Thrust density, on the other hand, is more commonly used in fluid dynamics to analyze the flow of fluids and how they interact with surfaces.

4. Can thrust and thrust density be used interchangeably?

No, thrust and thrust density cannot be used interchangeably as they measure different quantities. While thrust measures the overall force produced, thrust density takes into account the area over which the force is applied, providing a more specific measure of the force per unit area.

5. How do changes in thrust and thrust density affect performance?

Changes in thrust and thrust density can greatly affect the performance of a system. An increase in thrust can result in a faster acceleration, while an increase in thrust density can result in a more efficient use of the available power. However, these changes must be balanced with other factors such as weight and drag to achieve optimal performance.

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