Rocket Motor Guide
Qmodeling NIKEX
| 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 C6 | 13.83 | 2:1 | 6:1 | 147.61 | 30.65 | 5.6 | 1.34 | 1.20 | 2.34 | 63 |
| Aerotech E10 | 14.72 | 2:1 | 5:1 | 124.34 | 104.15 | 4.2 | 4.16 | 3.10 | 7.06 | 646 |
| Estes D11 | 14.88 | 3:1 | 7:1 | 182.05 | 52.55 | 3.4 | 1.94 | 2.20 | 3.94 | 165 |
| Apogee C10 | 13.92 | 3:1 | 7:1 | 184.38 | 32.35 | 4.2 | 0.97 | 1.40 | 2.17 | 59 |
| Aerotech D9W | 14.96 | 3:1 | 5:1 | 121.61 | 59.03 | 5.7 | 1.96 | 2.30 | 4.06 | 173 |
| Estes D12 | 14.80 | 3:1 | 8:1 | 212.02 | 52.62 | 3.0 | 1.72 | 2.30 | 3.82 | 156 |
| Aerotech C12T | 14.07 | 3:1 | 6:1 | 139.23 | 32.12 | 4.2 | 1.02 | 1.40 | 2.22 | 55 |
| Estes C11 | 14.54 | 3:1 | 6:1 | 145.51 | 30.96 | 4.9 | 0.82 | 1.40 | 2.02 | 45 |
| Aerotech E12RCJ | 15.39 | 3:1 | 5:1 | 115.88 | 100.19 | 4.5 | 3.11 | 3.40 | 6.31 | 512 |
| Aerotech D13W | 14.46 | 3:1 | 6:1 | 150.25 | 67.04 | 3.2 | 1.70 | 2.50 | 4.00 | 215 |
| Estes E15 | 15.45 | 3:1 | 5:1 | 130.78 | 89.82 | 5.1 | 2.65 | 3.50 | 5.95 | 388 |
| Aerotech E11J | 15.50 | 3:1 | 5:1 | 119.08 | 99.52 | 4.2 | 2.93 | 3.30 | 6.03 | 474 |
| Quest C12 Q-Jet | 14.13 | 3:1 | 5:1 | 97.98 | 34.20 | 5.8 | 0.86 | 1.60 | 2.26 | 54 |
| Aerotech D10W | 14.21 | 3:1 | 7:1 | 176.49 | 68.77 | 3.4 | 1.41 | 2.70 | 3.91 | 213 |
| Apogee D10 | 14.21 | 4:1 | 7:1 | 177.58 | 69.92 | 3.4 | 1.42 | 2.80 | 4.02 | 216 |
| Aerotech D15T | 14.85 | 4:1 | 8:1 | 194.40 | 69.70 | 2.6 | 1.46 | 2.60 | 3.86 | 216 |
| Aerotech F12 | 15.65 | 4:1 | 6:1 | 153.16 | 137.50 | 3.3 | 3.03 | 4.00 | 6.83 | 701 |
| Aerotech E15W | 15.07 | 4:1 | 8:1 | 200.25 | 125.98 | 2.7 | 2.68 | 4.10 | 6.58 | 640 |
| Quest D16 Q-Jet | 14.20 | 4:1 | 6:1 | 149.65 | 49.54 | 4.4 | 0.93 | 2.10 | 2.83 | 99 |
| Quest D20W Q-Jet | 14.15 | 5:1 | 7:1 | 174.36 | 55.27 | 4.0 | 0.85 | 2.30 | 2.95 | 118 |
| Aerotech C18W | 14.04 | 5:1 | 6:1 | 153.37 | 39.76 | 3.2 | 0.54 | 1.80 | 2.14 | 60 |
| Quest C18W Q-Jet | 14.04 | 5:1 | 6:1 | 153.37 | 39.76 | 3.2 | 0.54 | 1.80 | 2.14 | 60 |
| Aerotech E18W | 15.31 | 5:1 | 8:1 | 213.92 | 137.56 | 2.4 | 2.26 | 4.20 | 6.26 | 630 |
| Aerotech E20W | 15.03 | 5:1 | 9:1 | 245.22 | 128.49 | 2.1 | 1.80 | 4.20 | 5.80 | 527 |
| Aerotech D21T | 14.18 | 6:1 | 9:1 | 236.40 | 80.73 | 2.2 | 0.95 | 3.20 | 3.95 | 233 |
| Aerotech D24T | 14.39 | 6:1 | 11:1 | 177.99 | 64.93 | 3.3 | 0.92 | 2.70 | 3.42 | 162 |
| CTI 24E22-13A | 15.29 | 6:1 | 8:1 | 212.29 | 97.72 | 3.2 | 1.10 | 3.70 | 4.60 | 313 |
| Aerotech F24 | 15.50 | 6:1 | 11:1 | 286.92 | 160.37 | 2.0 | 2.16 | 4.70 | 6.66 | 758 |
| Aerotech E25T | 14.01 | 6:1 | 12:1 | 346.28 | 99.57 | 1.8 | 1.00 | 3.70 | 4.50 | 318 |
| Aerotech F30FJ | 15.77 | 8:1 | 10:1 | 260.07 | 181.65 | 2.1 | 1.67 | 5.10 | 6.57 | 758 |
| CTI 26E31-15A | 15.13 | 8:1 | 12:1 | 316.70 | 109.79 | 2.3 | 0.94 | 3.90 | 4.64 | 350 |
| Aerotech F32 | 15.59 | 8:1 | 16:1 | 406.10 | 235.70 | 1.4 | 1.89 | 5.80 | 7.49 | 1110 |
| Aerotech E30T | 14.83 | 9:1 | 13:1 | 363.12 | 162.42 | 1.5 | 1.29 | 4.80 | 5.89 | 628 |
| Aerotech E28T | 15.22 | 9:1 | 14:1 | 368.36 | 158.53 | 1.5 | 1.29 | 4.80 | 5.89 | 616 |
| Estes E30T | 14.81 | 9:1 | 13:1 | 370.20 | 136.86 | 1.6 | 1.10 | 4.50 | 5.40 | 488 |
| Aerotech F39 | 15.41 | 10:1 | 16:1 | 437.25 | 194.47 | 1.3 | 1.38 | 5.30 | 6.48 | 790 |
| Aerotech F44W | 14.99 | 12:1 | 18:1 | 488.04 | 184.52 | 1.5 | 1.04 | 5.10 | 5.94 | 651 |
| Aerotech E50 | 14.65 | 14:1 | 15:1 | 408.08 | 177.36 | 1.5 | 0.81 | 5.10 | 5.71 | 605 |
| CTI 25E75-17A | 15.13 | 20:1 | 26:1 | 723.29 | 105.04 | 1.1 | 0.36 | 3.90 | 4.06 | 282 |
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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