Rocket Motor Guide
Estes Rubicon
| 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 B4 | 7.97 | 2:1 | 6:1 | 157.90 | 20.14 | 18.3 | 1.12 | 0.90 | 1.82 | 30 |
| Weco C6 | 8.04 | 2:1 | 6:1 | 154.74 | 24.19 | 20.1 | 1.77 | 1.10 | 2.67 | 60 |
| Estes C6 | 8.12 | 2:1 | 7:1 | 178.14 | 42.93 | 8.5 | 1.92 | 1.80 | 3.52 | 119 |
| Estes B6 | 7.94 | 2:1 | 6:1 | 148.97 | 24.26 | 8.9 | 0.95 | 1.00 | 1.75 | 32 |
| Aerotech E6RCT | 9.16 | 3:1 | 6:1 | 130.62 | 66.55 | 3.8 | 7.26 | 2.50 | 8.76 | 683 |
| Aerotech E7RCT | 9.01 | 3:1 | 6:1 | 126.06 | 65.10 | 4.0 | 5.78 | 2.50 | 7.28 | 507 |
| Aerotech C6W | 8.11 | 3:1 | 6:1 | 137.75 | 56.67 | 3.7 | 1.61 | 1.90 | 3.31 | 148 |
| Quest B6 | 7.87 | 3:1 | 7:1 | 185.01 | 28.36 | 6.0 | 0.81 | 1.30 | 1.91 | 40 |
| Apogee E6 | 8.93 | 3:1 | 10:1 | 250.56 | 82.51 | 2.5 | 6.16 | 2.50 | 7.66 | 710 |
| Aerotech D7T | 8.79 | 3:1 | 5:1 | 118.01 | 69.91 | 4.1 | 2.92 | 2.40 | 5.12 | 325 |
| Apogee B7 | 7.62 | 3:1 | 7:1 | 194.67 | 31.63 | 3.2 | 0.83 | 1.30 | 1.93 | 47 |
| Aerotech D8 | 7.97 | 4:1 | 8:1 | 195.69 | 88.40 | 2.7 | 2.49 | 2.50 | 4.79 | 354 |
| Aerotech E10 | 8.72 | 4:1 | 10:1 | 233.13 | 145.29 | 2.5 | 4.12 | 2.50 | 6.42 | 724 |
| Estes D11 | 8.88 | 5:1 | 13:1 | 295.64 | 89.17 | 2.2 | 1.94 | 2.80 | 4.54 | 294 |
| Apogee C10 | 7.92 | 5:1 | 13:1 | 351.88 | 62.22 | 2.0 | 1.03 | 2.20 | 3.03 | 144 |
| Aerotech D9W | 8.96 | 5:1 | 10:1 | 219.21 | 103.39 | 4.1 | 1.97 | 2.80 | 4.57 | 310 |
| Estes D12 | 8.80 | 5:1 | 15:1 | 318.63 | 89.03 | 2.1 | 1.74 | 2.80 | 4.34 | 275 |
| Aerotech C12T | 8.07 | 5:1 | 10:1 | 268.46 | 61.66 | 2.1 | 0.98 | 2.20 | 2.98 | 138 |
| Estes C11 | 8.55 | 5:1 | 11:1 | 256.02 | 54.54 | 2.4 | 0.86 | 2.10 | 2.76 | 107 |
| Aerotech E12RCJ | 9.40 | 6:1 | 9:1 | 222.02 | 136.97 | 2.4 | 3.07 | 3.00 | 5.87 | 612 |
| Aerotech D13W | 8.47 | 6:1 | 11:1 | 284.95 | 109.85 | 1.8 | 1.71 | 2.80 | 4.31 | 336 |
| Aerotech E11J | 9.50 | 6:1 | 9:1 | 217.63 | 136.51 | 2.5 | 2.90 | 2.90 | 5.60 | 573 |
| Aerotech D10W | 8.22 | 6:1 | 12:1 | 335.43 | 113.03 | 2.0 | 1.41 | 3.00 | 4.21 | 331 |
| Apogee D10 | 8.22 | 7:1 | 12:1 | 337.38 | 114.87 | 2.0 | 1.42 | 3.00 | 4.22 | 335 |
| Aerotech D15T | 8.85 | 7:1 | 14:1 | 349.16 | 113.07 | 1.6 | 1.49 | 2.90 | 4.19 | 327 |
| Aerotech F12 | 9.65 | 7:1 | 12:1 | 267.75 | 168.55 | 1.9 | 2.93 | 3.20 | 5.93 | 715 |
| Aerotech E15W | 9.07 | 7:1 | 14:1 | 366.36 | 155.36 | 1.5 | 2.70 | 3.30 | 5.80 | 675 |
| Aerotech E18W | 9.31 | 9:1 | 15:1 | 385.73 | 181.39 | 1.4 | 2.30 | 3.30 | 5.40 | 637 |
| Aerotech E20W | 9.03 | 10:1 | 17:1 | 439.89 | 176.52 | 1.3 | 1.84 | 3.40 | 5.04 | 556 |
| Aerotech D21T | 8.18 | 10:1 | 16:1 | 441.63 | 132.35 | 1.3 | 0.99 | 3.30 | 4.09 | 333 |
| Aerotech D24T | 8.40 | 11:1 | 20:1 | 334.23 | 111.97 | 1.8 | 0.92 | 3.20 | 3.92 | 275 |
| CTI 24E22-13A | 9.29 | 11:1 | 15:1 | 382.89 | 154.83 | 1.9 | 1.11 | 3.60 | 4.51 | 406 |
| Aerotech F24 | 9.51 | 11:1 | 20:1 | 492.72 | 200.43 | 1.4 | 2.21 | 3.50 | 5.51 | 712 |
| Aerotech E25T | 8.01 | 11:1 | 22:1 | 643.65 | 157.13 | 1.0 | 0.95 | 3.50 | 4.25 | 392 |
| CTI 26E31-15A | 9.14 | 14:1 | 22:1 | 561.60 | 171.11 | 1.4 | 0.88 | 3.80 | 4.48 | 424 |
| Aerotech E30T | 8.83 | 16:1 | 24:1 | 653.62 | 220.29 | 1.0 | 1.26 | 3.80 | 4.86 | 589 |
| Aerotech E28T | 9.22 | 16:1 | 25:1 | 625.75 | 213.20 | 1.0 | 1.26 | 3.80 | 4.86 | 589 |
| Estes E30T | 8.81 | 16:1 | 24:1 | 665.00 | 193.68 | 1.0 | 1.05 | 3.70 | 4.55 | 499 |
| Aerotech F39 | 9.42 | 18:1 | 29:1 | 749.44 | 243.45 | 0.9 | 1.35 | 4.00 | 5.15 | 689 |
| Aerotech F44W | 8.99 | 21:1 | 32:1 | 849.27 | 269.54 | 1.2 | 1.01 | 3.90 | 4.71 | 586 |
| Aerotech E50 | 8.66 | 26:1 | 27:1 | 689.35 | 270.09 | 1.0 | 0.87 | 4.00 | 4.67 | 586 |
| CTI 25E75-17A | 9.14 | 37:1 | 47:1 | 1251.65 | 166.99 | 0.7 | 0.33 | 3.70 | 3.83 | 330 |
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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