OpenRocket variability

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Macrophage42

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So I ran a simulation with a rocket and a motor and got a result. I then ran the simulation again, and the apogee altitude was a few meters different. I ran it again, and got another different but close apogee result.

Is there some sort of variability built into the simulation, or am I using it incorrectly?
 
So I ran a simulation with a rocket and a motor and got a result. I then ran the simulation again, and the apogee altitude was a few meters different. I ran it again, and got another different but close apogee result.

Is there some sort of variability built into the simulation, or am I using it incorrectly?

I've not had that issue? Perhaps post up the .ork file so the folks can take a look at it.
 
There are non-zero values for average wind speed and std. deviation, so that must be it. Thanks.
 
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