Anthony replied to Eric:
> > RL rocket thrust equations are in the realm of calculus
> 
> Unless you've got more going on than just changes in ship mass as one 
> expels fuel, it's extremely basic calculus -- delta-V = exhaust velocity 
> * ln( loaded mass / empty mass )

... which is just about what Vehicles Expansion 2 says, give 
or take a few equivalencies.

Regards,
Onno
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