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Rocket
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Apogee Determination
Performance Prediction
Drag Prediction
Drag Estimate
Drag Estimate (Under Development)
Engine Total Impulse:
n-s
Engine Thrust Duration:
s
Engine Initial Mass:
g
Engine Propellant Mass:
g
Rocket Mass (no engine):
g
Rocket Diameter:
cm
Coast Time:
s
Measured Apogee Altitude:
m
Calculate
Results
Burnout Altitude:
m
Burnout Velocity:
m/s
Coast Distance:
m
Total Altitude:
m
Estimated Drag Coefficient:
Created By:
Dennis Hawk &
Dustin Griffith