Rocket Motor Guide
Semroc AIM-54C Phoenix
Semroc - AIM-54C Phoenix {Kit} (KD-6) [2013-2013]
| 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 |
|---|---|---|---|---|---|---|---|---|---|---|
| Apogee A2 | 2.04 | 4:1 | 10:1 | 256.70 | 60.81 | 4.6 | 1.40 | 2.30 | 3.50 | 152 |
| Apogee 1/2A2 | 1.95 | 4:1 | 8:1 | 209.27 | 31.33 | 4.8 | 0.71 | 1.40 | 1.91 | 45 |
| Estes A3T | 2.10 | 4:1 | 12:1 | 307.56 | 57.10 | 2.1 | 1.10 | 2.10 | 3.00 | 126 |
| Estes A10T | 1.98 | 5:1 | 25:1 | 626.94 | 37.58 | 1.3 | 0.94 | 1.50 | 2.24 | 68 |
| MPC 1/2A3-M | 2.03 | 6:1 | 10:1 | 263.15 | 27.96 | 2.3 | 0.52 | 1.20 | 1.52 | 31 |
| Estes 1/2A3T | 2.03 | 6:1 | 15:1 | 416.25 | 26.86 | 1.5 | 0.45 | 1.20 | 1.45 | 29 |
| Quest C6 | 2.66 | 6:1 | 31:1 | 661.00 | 125.85 | 2.0 | 2.61 | 3.50 | 5.91 | 604 |
| Estes A8 | 2.37 | 6:1 | 19:1 | 423.55 | 46.74 | 1.7 | 0.80 | 1.90 | 2.50 | 86 |
| Estes 1/2A6 | 2.29 | 7:1 | 16:1 | 365.88 | 20.25 | 1.9 | 0.41 | 0.90 | 1.11 | 15 |
| Apogee C4 | 2.40 | 8:1 | 23:1 | 510.76 | 130.64 | 1.5 | 2.41 | 3.60 | 5.81 | 637 |
| Estes C5 | 2.54 | 8:1 | 41:1 | 981.88 | 163.70 | 1.3 | 2.03 | 3.80 | 5.63 | 653 |
| Estes B4 | 2.47 | 8:1 | 26:1 | 601.21 | 92.78 | 1.3 | 1.03 | 3.10 | 3.93 | 243 |
| Weco C6 | 2.54 | 9:1 | 25:1 | 442.01 | 123.89 | 1.6 | 1.74 | 3.50 | 5.04 | 432 |
| Estes C6 | 2.61 | 9:1 | 28:1 | 529.46 | 162.03 | 1.4 | 1.95 | 3.80 | 5.55 | 580 |
| Estes B6 | 2.44 | 10:1 | 24:1 | 502.39 | 101.95 | 1.5 | 0.95 | 3.10 | 3.85 | 255 |
| Quest A6 | 2.34 | 10:1 | 24:1 | 439.91 | 46.02 | 1.7 | 0.46 | 1.90 | 2.16 | 70 |
| Quest A8 Q-Jet | 2.26 | 10:1 | 22:1 | 442.64 | 50.53 | 1.8 | 0.39 | 2.00 | 2.19 | 74 |
| FSI A6 | 2.37 | 11:1 | 23:1 | 452.66 | 45.68 | 1.5 | 0.54 | 1.70 | 2.04 | 63 |
| Aerotech C6W | 2.61 | 12:1 | 24:1 | 512.99 | 195.32 | 1.5 | 1.63 | 3.90 | 5.33 | 629 |
| Quest B6 | 2.37 | 12:1 | 29:1 | 503.30 | 118.42 | 1.5 | 0.83 | 3.30 | 3.93 | 287 |
| Apogee B7 | 2.12 | 13:1 | 30:1 | 639.87 | 132.16 | 1.3 | 0.78 | 3.40 | 3.98 | 325 |
| Aerotech D8 | 2.47 | 14:1 | 31:1 | 761.46 | 282.01 | 1.0 | 2.47 | 3.90 | 6.17 | 1052 |
| Apogee C10 | 2.42 | 20:1 | 51:1 | 1291.90 | 210.54 | 0.7 | 1.05 | 4.00 | 4.85 | 571 |
| Aerotech C12T | 2.57 | 22:1 | 41:1 | 862.57 | 206.76 | 1.1 | 0.99 | 4.20 | 4.99 | 567 |
| Aerotech D13W | 2.96 | 23:1 | 45:1 | 951.62 | 306.94 | 0.7 | 1.74 | 4.40 | 5.94 | 968 |
| Aerotech D10W | 2.71 | 25:1 | 50:1 | 1189.60 | 323.59 | 0.7 | 1.43 | 4.40 | 5.63 | 933 |
| Apogee D10 | 2.71 | 27:1 | 50:1 | 1196.35 | 327.23 | 0.7 | 1.44 | 4.40 | 5.64 | 937 |
| Aerotech D21T | 2.68 | 42:1 | 64:1 | 1554.37 | 379.89 | 0.6 | 1.04 | 4.60 | 5.44 | 901 |
| Aerotech D24T | 2.89 | 44:1 | 83:1 | 1122.54 | 320.95 | 0.7 | 0.94 | 4.80 | 5.54 | 840 |
| Aerotech E25T | 2.51 | 47:1 | 89:1 | 2344.10 | 441.80 | 0.5 | 1.02 | 4.40 | 5.22 | 963 |
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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