Maximum delta-v of a rocket engine

Join the discussion
Registration is free. Ask a follow-up in this thread, or start your own.
5 replies · 2K views
yrjosmiel
Messages
53
Reaction score
5
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
 
Last edited by a moderator:
Physics news on Phys.org
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.
 
  • Like
Likes   Reactions: mfb