Estes Flutter-By
Estes - Flutter-By {Kit} (003013)
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 | 1.23 | 7:1 | 17:1 | 461.41 | 118.93 | 1.7 | 1.34 | 3.70 | 4.84 | 373 |
Apogee 1/2A2 | 1.15 | 7:1 | 14:1 | 384.70 | 65.03 | 2.0 | 0.65 | 2.50 | 2.95 | 134 |
Estes A3T | 1.30 | 8:1 | 21:1 | 537.37 | 102.62 | 1.3 | 1.05 | 3.40 | 4.25 | 290 |
Estes A10T | 1.19 | 8:1 | 46:1 | 762.15 | 73.08 | 1.1 | 0.92 | 2.70 | 3.42 | 181 |
Estes 1/4A3T | 1.21 | 9:1 | 18:1 | 450.32 | 20.26 | 1.5 | 0.34 | 0.90 | 1.04 | 14 |
Apogee 1/4A2 | 1.13 | 9:1 | 19:1 | 536.25 | 21.37 | 1.3 | 0.32 | 1.00 | 1.12 | 17 |
MPC 1/2A3-M | 1.23 | 11:1 | 18:1 | 404.84 | 52.12 | 1.7 | 0.46 | 2.20 | 2.46 | 87 |
Estes 1/2A3T | 1.23 | 11:1 | 27:1 | 660.18 | 45.31 | 1.2 | 0.42 | 1.90 | 2.12 | 69 |
Quest C6 | 1.86 | 11:1 | 56:1 | 935.35 | 211.94 | 1.8 | 2.57 | 5.10 | 7.47 | 1158 |
Estes A8 | 1.57 | 11:1 | 35:1 | 516.26 | 80.27 | 1.5 | 0.77 | 3.10 | 3.67 | 203 |
Estes 1/2A6 | 1.49 | 12:1 | 28:1 | 480.49 | 37.10 | 1.6 | 0.38 | 1.70 | 1.88 | 46 |
Apogee C4 | 1.60 | 14:1 | 41:1 | 793.40 | 214.83 | 1.1 | 2.38 | 5.00 | 7.18 | 1160 |
Estes C5 | 1.74 | 14:1 | 74:1 | 1667.32 | 268.51 | 1.1 | 2.00 | 5.20 | 7.00 | 1188 |
Estes B4 | 1.66 | 15:1 | 46:1 | 769.92 | 148.06 | 1.1 | 1.11 | 4.30 | 5.21 | 495 |
Weco C6 | 1.74 | 17:1 | 45:1 | 929.96 | 211.22 | 1.3 | 1.81 | 4.80 | 6.41 | 850 |
Estes C6 | 1.81 | 17:1 | 51:1 | 652.45 | 267.33 | 1.2 | 1.93 | 5.30 | 7.03 | 1102 |
Estes B6 | 1.64 | 18:1 | 44:1 | 615.85 | 164.16 | 1.3 | 0.93 | 4.50 | 5.23 | 524 |
Quest A6 | 1.54 | 18:1 | 43:1 | 623.35 | 79.24 | 1.4 | 0.43 | 3.00 | 3.23 | 173 |
Quest A8 Q-Jet | 1.46 | 18:1 | 40:1 | 873.75 | 89.43 | 1.5 | 0.45 | 3.20 | 3.45 | 200 |
FSI A6 | 1.57 | 20:1 | 41:1 | 824.96 | 76.48 | 1.3 | 0.51 | 2.80 | 3.11 | 156 |
Aerotech C6W | 1.81 | 22:1 | 42:1 | 784.96 | 304.25 | 1.3 | 1.71 | 5.40 | 6.91 | 1145 |
Quest B6 | 1.57 | 22:1 | 52:1 | 815.83 | 199.28 | 1.2 | 0.80 | 4.70 | 5.30 | 594 |
Apogee B7 | 1.32 | 24:1 | 53:1 | 1147.61 | 226.13 | 0.9 | 0.75 | 4.70 | 5.25 | 640 |
Aerotech D8 | 1.67 | 26:1 | 55:1 | 1239.48 | 456.35 | 0.8 | 2.45 | 5.30 | 7.55 | 1806 |
Apogee C10 | 1.62 | 36:1 | 93:1 | 2024.95 | 332.71 | 0.6 | 1.04 | 5.40 | 6.24 | 1033 |
Aerotech C12T | 1.77 | 39:1 | 74:1 | 1346.36 | 323.38 | 1.0 | 0.97 | 5.70 | 6.47 | 1048 |
Aerotech D13W | 2.16 | 41:1 | 80:1 | 1385.25 | 468.42 | 0.6 | 1.73 | 6.10 | 7.63 | 1717 |
Aerotech D10W | 1.91 | 45:1 | 90:1 | 1814.29 | 505.62 | 0.5 | 1.42 | 6.00 | 7.22 | 1639 |
Apogee D10 | 1.91 | 48:1 | 91:1 | 1824.44 | 512.16 | 0.6 | 1.43 | 6.00 | 7.23 | 1653 |
Aerotech D21T | 1.88 | 75:1 | 116:1 | 2378.52 | 591.89 | 0.5 | 1.03 | 6.10 | 6.93 | 1582 |
Aerotech D24T | 2.09 | 79:1 | 149:1 | 1449.39 | 491.97 | 0.6 | 0.93 | 6.50 | 7.23 | 1494 |
Aerotech E25T | 1.71 | 84:1 | 161:1 | 3586.05 | 703.52 | 0.4 | 1.01 | 5.80 | 6.61 | 1641 |
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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