Rocket Motor Guide
Estes Photon Disruptor
Estes - Photon Disruptor {Kit} (003025) [2010-]
| 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 | 2.63 | 3:1 | 7:1 | 188.33 | 46.09 | 7.6 | 1.37 | 2.00 | 3.17 | 107 |
| Apogee 1/2A2 | 2.55 | 3:1 | 6:1 | 151.50 | 23.86 | 7.6 | 0.68 | 1.10 | 1.58 | 27 |
| Estes A3T | 2.70 | 3:1 | 9:1 | 228.97 | 42.82 | 4.5 | 1.01 | 1.90 | 2.71 | 86 |
| Estes A10T | 2.58 | 4:1 | 19:1 | 535.56 | 30.46 | 1.4 | 0.86 | 1.40 | 2.06 | 51 |
| MPC 1/2A3-M | 2.63 | 5:1 | 8:1 | 194.35 | 21.52 | 3.8 | 0.50 | 1.00 | 1.30 | 20 |
| Estes 1/2A3T | 2.63 | 5:1 | 11:1 | 311.82 | 24.36 | 2.5 | 0.40 | 1.10 | 1.30 | 23 |
| Quest C6 | 3.26 | 5:1 | 23:1 | 562.94 | 120.88 | 2.1 | 2.63 | 3.90 | 6.33 | 606 |
| Estes A8 | 2.98 | 5:1 | 15:1 | 355.12 | 39.05 | 1.9 | 0.82 | 1.70 | 2.32 | 66 |
| Estes 1/2A6 | 2.89 | 5:1 | 12:1 | 292.43 | 20.14 | 2.1 | 0.34 | 1.00 | 1.14 | 13 |
| Apogee C4 | 3.00 | 6:1 | 17:1 | 409.28 | 128.40 | 1.8 | 2.43 | 4.10 | 6.33 | 654 |
| Estes C5 | 3.14 | 6:1 | 31:1 | 696.54 | 157.65 | 1.4 | 2.04 | 4.40 | 6.24 | 696 |
| Estes B4 | 3.07 | 6:1 | 19:1 | 483.95 | 77.02 | 1.4 | 1.05 | 3.00 | 3.85 | 213 |
| Weco C6 | 3.14 | 7:1 | 19:1 | 388.77 | 107.75 | 1.8 | 1.76 | 3.70 | 5.26 | 407 |
| Estes C6 | 3.21 | 7:1 | 21:1 | 462.10 | 150.28 | 1.6 | 1.87 | 4.40 | 6.07 | 604 |
| Estes B6 | 3.04 | 8:1 | 18:1 | 452.84 | 84.03 | 1.6 | 0.87 | 3.20 | 3.87 | 224 |
| Quest A6 | 2.94 | 8:1 | 18:1 | 397.76 | 35.02 | 1.8 | 0.48 | 1.60 | 1.88 | 47 |
| Quest A8 Q-Jet | 2.86 | 8:1 | 17:1 | 333.07 | 32.58 | 2.0 | 0.41 | 1.50 | 1.71 | 37 |
| FSI A6 | 2.97 | 8:1 | 17:1 | 383.10 | 24.91 | 1.7 | 0.56 | 1.00 | 1.36 | 23 |
| Aerotech C6W | 3.21 | 9:1 | 18:1 | 414.81 | 175.31 | 1.7 | 1.65 | 4.60 | 6.05 | 690 |
| Quest B6 | 2.97 | 9:1 | 22:1 | 456.67 | 96.64 | 1.6 | 0.85 | 3.40 | 4.05 | 256 |
| Apogee B7 | 2.72 | 10:1 | 22:1 | 618.34 | 108.89 | 1.3 | 0.79 | 3.60 | 4.19 | 314 |
| Aerotech D8 | 3.07 | 11:1 | 23:1 | 598.43 | 262.32 | 1.1 | 2.48 | 5.00 | 7.28 | 1254 |
| Apogee C10 | 3.02 | 15:1 | 39:1 | 1013.26 | 184.93 | 0.8 | 1.06 | 4.70 | 5.56 | 635 |
| Aerotech C12T | 3.17 | 16:1 | 31:1 | 673.02 | 180.19 | 1.2 | 1.00 | 4.80 | 5.60 | 620 |
| Aerotech D13W | 3.56 | 17:1 | 33:1 | 768.26 | 294.41 | 0.9 | 1.74 | 5.40 | 6.94 | 1167 |
| Aerotech D10W | 3.31 | 19:1 | 38:1 | 942.90 | 310.42 | 0.8 | 1.44 | 5.50 | 6.74 | 1144 |
| Apogee D10 | 3.31 | 20:1 | 38:1 | 948.12 | 313.88 | 0.8 | 1.44 | 5.50 | 6.74 | 1150 |
| Aerotech D21T | 3.28 | 31:1 | 48:1 | 1231.21 | 361.70 | 0.6 | 0.94 | 5.80 | 6.54 | 1130 |
| Aerotech D24T | 3.49 | 33:1 | 62:1 | 903.71 | 304.34 | 0.8 | 0.95 | 5.80 | 6.55 | 1018 |
| Aerotech E25T | 3.11 | 35:1 | 67:1 | 1860.13 | 428.02 | 0.5 | 1.02 | 5.70 | 6.52 | 1245 |
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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