Multiple Stage Model Rocket Simulator

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A simulation of "N" identical stages.
N=Newtons; s=Seconds; g=grams; kg=kilograms; m=meters; mm=millimeters; MSL=mean sea level; inHg=inches of mercury
Select engine profile Number of stages Weight, in excess of engine case and propellant, released at each staging(g)
Ejection Delay(s) Payload weight(g) Frontal Diameter(mm)
Coefficient of Drag(No Units) Barometer at MSL (inHg) Initial Elevation(m)
(const) Acceleration Due To Gravity defined (m/s^2) (const) Air Density at 1 atm defined (kg/m^3) (const) 1 atm defined (inHg)
Note: Ejection Delay is not currently used in the simulation.
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