Rocket Motor Guide
Rocketarium Cerberus
Rocketarium - Cerberus {Kit} (RK-1002)
| Motor | Weight oz | TTW Average | TTW Peak | Accel f/s2 | Speed mph | Rod Len feet | Burnout Time sec | Optimal Delay sec | Time to Apogee sec | Altitude feet |
|---|---|---|---|---|---|---|---|---|---|---|
| Estes A3T | 3.90 | 2:1 | 6:1 | 146.04 | 24.19 | 12.8 | 1.04 | 1.10 | 1.94 | 36 |
| Estes A10T | 3.79 | 2:1 | 13:1 | 367.54 | 22.73 | 1.8 | 0.90 | 1.10 | 1.80 | 35 |
| Quest C6 | 4.46 | 3:1 | 15:1 | 343.70 | 81.02 | 2.3 | 2.57 | 3.10 | 5.47 | 372 |
| Estes A8 | 4.18 | 3:1 | 10:1 | 244.38 | 27.40 | 3.1 | 0.79 | 1.20 | 1.79 | 39 |
| Apogee C4 | 4.20 | 4:1 | 11:1 | 276.69 | 87.39 | 2.4 | 2.38 | 3.20 | 5.38 | 411 |
| Estes C5 | 4.35 | 4:1 | 20:1 | 457.34 | 108.08 | 1.6 | 2.07 | 3.60 | 5.47 | 445 |
| Estes B4 | 4.27 | 4:1 | 13:1 | 331.14 | 54.44 | 1.8 | 1.08 | 2.30 | 3.18 | 130 |
| Weco C6 | 4.34 | 5:1 | 12:1 | 322.27 | 68.97 | 2.1 | 1.80 | 2.70 | 4.30 | 228 |
| Estes C6 | 4.42 | 5:1 | 14:1 | 370.64 | 106.21 | 1.8 | 1.90 | 3.70 | 5.40 | 401 |
| Estes B6 | 4.24 | 5:1 | 12:1 | 314.39 | 57.34 | 1.9 | 0.90 | 2.40 | 3.10 | 129 |
| Quest A6 | 4.14 | 5:1 | 12:1 | 307.31 | 25.84 | 2.1 | 0.42 | 1.20 | 1.42 | 25 |
| Quest A8 Q-Jet | 4.06 | 5:1 | 11:1 | 288.71 | 21.38 | 2.4 | 0.46 | 1.00 | 1.26 | 18 |
| FSI A6 | 4.17 | 5:1 | 11:1 | 289.68 | 20.22 | 2.1 | 0.50 | 0.80 | 1.10 | 13 |
| Aerotech C6W | 4.41 | 6:1 | 12:1 | 287.73 | 124.06 | 2.1 | 1.69 | 3.80 | 5.29 | 458 |
| Quest B6 | 4.17 | 6:1 | 14:1 | 385.75 | 65.53 | 1.8 | 0.78 | 2.60 | 3.18 | 149 |
| Apogee B7 | 3.92 | 7:1 | 15:1 | 414.02 | 71.47 | 1.6 | 0.82 | 2.70 | 3.32 | 175 |
| Aerotech D8 | 4.27 | 7:1 | 15:1 | 408.49 | 188.77 | 1.5 | 2.51 | 4.40 | 6.71 | 928 |
| Apogee C10 | 4.22 | 10:1 | 26:1 | 702.78 | 130.98 | 1.0 | 0.97 | 4.10 | 4.87 | 426 |
| Aerotech C12T | 4.37 | 11:1 | 21:1 | 514.23 | 127.91 | 1.4 | 1.02 | 4.00 | 4.82 | 410 |
| Aerotech D13W | 4.77 | 11:1 | 22:1 | 550.43 | 219.47 | 1.1 | 1.76 | 4.80 | 6.36 | 863 |
| Aerotech D10W | 4.52 | 12:1 | 25:1 | 661.64 | 232.00 | 1.1 | 1.46 | 5.00 | 6.26 | 860 |
| Apogee D10 | 4.52 | 13:1 | 25:1 | 665.33 | 231.66 | 1.1 | 1.46 | 5.00 | 6.26 | 857 |
| Aerotech D21T | 4.48 | 21:1 | 32:1 | 864.60 | 266.10 | 0.8 | 0.95 | 5.30 | 6.05 | 850 |
| Aerotech D24T | 4.69 | 22:1 | 41:1 | 645.42 | 226.09 | 1.0 | 0.96 | 5.20 | 5.96 | 752 |
| Aerotech E25T | 4.31 | 23:1 | 45:1 | 1280.57 | 316.75 | 0.6 | 1.03 | 5.30 | 6.13 | 964 |
Weight - The total weight of the rocket, with motor, at lift-off.
TTW Average - The average thrust-to-weight ratio of the rocket.
TTW Peak - The peak thrust-to-weight ratio of the rocket.
Accel - The maximum acceleration experienced by the rocket.
Speed - The maximum speed experienced by the rocket.
Rod Len - The minimal rod/rail length for the rocket to reach a safe speed (9 m/s) for free flight.
Optimal Delay - The optimal delay time (equal to the time from burnout to apogee).
Altitude - The altitude at apogee.
Note: These simulation results should be used with caution. Always double-check to ensure that your flight will be safe.
The Rocket Motor Guide helps you choose the right motor to use in your rocket by running a simulation using each of the motors in the RocketReviews.com motor database.
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