74.65 m (244 feet)

Motor Equivalent

Crashdown

Acceleration

Burn Time

60.95 m/s

Burnout

-4 m/s

3.36 s

0.07 s

4.58 m

0.10 s

Time

Time

D232

232 N

Time

Simulation

Average Thrust

Total Impulse

Peak Thrust

18.66 s

Velocity

Altitude

Apogee

572.71 N

16.79 Ns

Thrust

-5.71 G

Velocity

Altitude

This page presents the results from my water bottle rocket simulations using the tool provided by Air Command Rockets. I used this simulator to model different rocket parameters—such as water volume, pressure, nozzle size, and drag coefficient—to predict how these changes would influence altitude, thrust, and flight duration. These simulations helped guide design decisions before physical testing, allowing me to optimize the rocket’s performance and understand key relationships between the variables at play.

DEVELOPMENT

CAD
CODE
REPORT

RESEARCH

WINDTUNNEL
TESTING
CONCLUSIONS
SIMULATION
CALCULATIONS
MARKET