Maximum delta-v of a rocket engine

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The discussion focuses on calculating the maximum delta-v of a rocket engine using the rocket equation, which requires determining the exhaust velocity and making assumptions about the dry mass fraction. Participants note that these calculations are often estimates rather than precise measurements. The conversation highlights the importance of mass fraction, especially in hybrid rockets where the integrity of solid fuel decreases significantly as it burns. Additionally, it mentions that tether propulsion does not adhere to the rocket equation. Overall, understanding these concepts is crucial for accurate propulsion analysis in rocketry.
yrjosmiel
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So I was browsing wikipedia when I encountered:
qB8vCyTfQw25KlsN_gXyZA.png

What does this exactly mean? How does one calculate for this?

<< Adding link to the table >> https://en.wikipedia.org/wiki/Spacecraft_propulsion#Table_of_methods
 
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Find the exhaust velocity, then make reasonable assumptions about the dry mass fraction and use the rocket equation.
 
mfb said:
Find the exhaust velocity, then make reasonable assumptions about the dry mass fraction and use the rocket equation.
So it's more or less an estimate?
 
yrjosmiel said:
So it's more or less an estimate?
Something cool about engineer. A lot of "measurements" are really just estimates.

Look at gps guidance in your car.
 
Note that tether propulsion does not conform to the rocket equation at all.
For hybrid rockets, the mass fraction is critical, as in most cases a solid fuel is burned using an injected oxidizer.
The fuel loses integrity once 80 or so percent have burnt, which kills the mass fraction.
 
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Due to the constant never ending supply of "cool stuff" happening in Aerospace these days I'm creating this thread to consolidate posts every time something new comes along. Please feel free to add random information if its relevant. So to start things off here is the SpaceX Dragon launch coming up shortly, I'll be following up afterwards to see how it all goes. :smile: https://blogs.nasa.gov/spacex/

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