Rocket Motor Guide
Estes Trident
Estes - Trident {Kit} (K-33) [?-?]
| 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 | 2.91 | 3:1 | 6:1 | 166.99 | 40.23 | 9.3 | 1.36 | 1.80 | 2.96 | 90 |
| Apogee 1/2A2 | 2.83 | 3:1 | 5:1 | 133.54 | 20.15 | 9.0 | 0.67 | 1.00 | 1.47 | 20 |
| Estes A3T | 2.97 | 3:1 | 8:1 | 204.21 | 36.77 | 6.0 | 1.08 | 1.70 | 2.58 | 74 |
| Estes A10T | 2.85 | 3:1 | 17:1 | 504.62 | 28.63 | 1.5 | 0.87 | 1.30 | 1.97 | 48 |
| MPC 1/2A3-M | 2.90 | 4:1 | 7:1 | 172.76 | 20.17 | 4.8 | 0.45 | 1.00 | 1.25 | 16 |
| Estes 1/2A3T | 2.90 | 4:1 | 10:1 | 279.04 | 20.14 | 3.7 | 0.45 | 0.90 | 1.15 | 17 |
| Quest C6 | 3.53 | 4:1 | 21:1 | 513.89 | 125.65 | 2.2 | 2.54 | 4.70 | 7.04 | 687 |
| Estes A8 | 3.25 | 4:1 | 13:1 | 326.93 | 36.67 | 1.9 | 0.83 | 1.60 | 2.23 | 61 |
| Estes 1/2A6 | 3.16 | 5:1 | 11:1 | 264.20 | 20.24 | 2.3 | 0.36 | 1.00 | 1.16 | 14 |
| Apogee C4 | 3.27 | 5:1 | 15:1 | 377.29 | 137.18 | 1.9 | 2.44 | 4.90 | 7.14 | 772 |
| Estes C5 | 3.41 | 5:1 | 28:1 | 602.67 | 163.30 | 1.4 | 2.05 | 5.50 | 7.35 | 846 |
| Estes B4 | 3.34 | 6:1 | 17:1 | 439.59 | 72.34 | 1.5 | 1.05 | 3.10 | 3.95 | 210 |
| Weco C6 | 3.41 | 6:1 | 17:1 | 369.53 | 103.41 | 1.8 | 1.77 | 4.10 | 5.67 | 430 |
| Estes C6 | 3.49 | 6:1 | 19:1 | 439.92 | 151.44 | 1.6 | 1.87 | 5.30 | 6.97 | 718 |
| Estes B6 | 3.31 | 7:1 | 16:1 | 418.26 | 78.60 | 1.6 | 0.88 | 3.30 | 3.98 | 224 |
| Quest A6 | 3.21 | 7:1 | 16:1 | 381.50 | 31.66 | 1.9 | 0.49 | 1.50 | 1.79 | 41 |
| Quest A8 Q-Jet | 3.13 | 7:1 | 15:1 | 314.72 | 28.65 | 2.1 | 0.42 | 1.30 | 1.52 | 31 |
| FSI A6 | 3.24 | 7:1 | 15:1 | 357.27 | 22.03 | 1.8 | 0.47 | 0.90 | 1.17 | 19 |
| Aerotech C6W | 3.48 | 8:1 | 16:1 | 378.63 | 174.75 | 1.8 | 1.66 | 5.60 | 7.06 | 857 |
| Quest B6 | 3.24 | 8:1 | 19:1 | 438.16 | 89.06 | 1.7 | 0.76 | 3.60 | 4.16 | 261 |
| Apogee B7 | 2.99 | 9:1 | 20:1 | 557.90 | 100.39 | 1.4 | 0.80 | 3.90 | 4.50 | 328 |
| Aerotech D8 | 3.34 | 10:1 | 21:1 | 547.96 | 289.29 | 1.2 | 2.49 | 6.90 | 9.19 | 1784 |
| Apogee C10 | 3.29 | 13:1 | 35:1 | 922.32 | 181.40 | 0.8 | 1.06 | 5.70 | 6.56 | 795 |
| Aerotech C12T | 3.44 | 14:1 | 28:1 | 611.05 | 176.11 | 1.3 | 1.01 | 5.80 | 6.61 | 763 |
| Aerotech D13W | 3.83 | 15:1 | 30:1 | 705.95 | 310.41 | 0.9 | 1.75 | 7.30 | 8.85 | 1654 |
| Aerotech D10W | 3.58 | 17:1 | 34:1 | 861.23 | 331.07 | 0.9 | 1.44 | 7.50 | 8.74 | 1653 |
| Apogee D10 | 3.58 | 18:1 | 34:1 | 865.93 | 334.05 | 0.9 | 1.45 | 7.50 | 8.75 | 1661 |
| Aerotech D21T | 3.55 | 28:1 | 43:1 | 1124.53 | 371.74 | 0.7 | 0.95 | 7.80 | 8.55 | 1662 |
| Aerotech D24T | 3.76 | 29:1 | 56:1 | 829.84 | 308.62 | 0.9 | 0.95 | 7.60 | 8.35 | 1428 |
| Aerotech E25T | 3.38 | 31:1 | 60:1 | 1689.01 | 454.43 | 0.6 | 1.02 | 7.90 | 8.72 | 1907 |
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.
Sponsored Ads
 |
 |