Estes Bandit
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 | 2.84 | 3:1 | 7:1 | 172.13 | 40.91 | 8.8 | 1.34 | 1.90 | 3.04 | 91 |
Apogee 1/2A2 | 2.75 | 3:1 | 5:1 | 137.86 | 20.16 | 8.6 | 0.65 | 1.00 | 1.45 | 20 |
Estes A3T | 2.90 | 3:1 | 8:1 | 210.19 | 39.74 | 5.6 | 1.06 | 1.80 | 2.66 | 81 |
Estes A10T | 2.79 | 3:1 | 18:1 | 511.46 | 29.08 | 1.4 | 0.86 | 1.40 | 2.06 | 49 |
MPC 1/2A3-M | 2.83 | 4:1 | 7:1 | 177.99 | 20.17 | 4.5 | 0.44 | 1.00 | 1.24 | 16 |
Estes 1/2A3T | 2.83 | 4:1 | 11:1 | 286.97 | 21.35 | 3.3 | 0.44 | 1.00 | 1.24 | 20 |
Quest C6 | 3.46 | 4:1 | 21:1 | 528.59 | 127.69 | 2.2 | 2.64 | 4.60 | 7.04 | 697 |
Estes A8 | 3.17 | 4:1 | 13:1 | 335.14 | 37.39 | 1.9 | 0.83 | 1.60 | 2.23 | 63 |
Estes 1/2A6 | 3.09 | 5:1 | 11:1 | 271.14 | 20.18 | 2.2 | 0.35 | 1.00 | 1.15 | 14 |
Apogee C4 | 3.20 | 5:1 | 16:1 | 385.43 | 138.90 | 1.9 | 2.44 | 4.90 | 7.14 | 777 |
Estes C5 | 3.34 | 5:1 | 28:1 | 622.87 | 165.85 | 1.4 | 2.05 | 5.40 | 7.25 | 849 |
Estes B4 | 3.27 | 6:1 | 18:1 | 450.45 | 73.85 | 1.4 | 1.05 | 3.10 | 3.95 | 216 |
Weco C6 | 3.34 | 7:1 | 17:1 | 374.39 | 106.00 | 1.8 | 1.77 | 4.10 | 5.67 | 441 |
Estes C6 | 3.41 | 7:1 | 20:1 | 444.77 | 153.83 | 1.6 | 1.87 | 5.30 | 6.97 | 721 |
Estes B6 | 3.24 | 7:1 | 17:1 | 428.63 | 80.43 | 1.7 | 0.88 | 3.30 | 3.98 | 231 |
Quest A6 | 3.14 | 7:1 | 16:1 | 385.77 | 32.49 | 1.9 | 0.49 | 1.50 | 1.79 | 43 |
Quest A8 Q-Jet | 3.06 | 7:1 | 15:1 | 320.03 | 29.57 | 2.1 | 0.42 | 1.40 | 1.62 | 32 |
FSI A6 | 3.17 | 8:1 | 16:1 | 363.94 | 22.53 | 1.8 | 0.47 | 1.00 | 1.27 | 20 |
Aerotech C6W | 3.41 | 8:1 | 16:1 | 387.56 | 177.59 | 1.8 | 1.66 | 5.60 | 7.06 | 857 |
Quest B6 | 3.17 | 9:1 | 20:1 | 441.93 | 91.16 | 1.7 | 0.76 | 3.70 | 4.26 | 267 |
Apogee B7 | 2.92 | 9:1 | 20:1 | 572.60 | 103.24 | 1.4 | 0.79 | 4.00 | 4.59 | 337 |
Aerotech D8 | 3.27 | 10:1 | 21:1 | 561.47 | 288.86 | 1.2 | 2.49 | 6.70 | 8.99 | 1746 |
Apogee C10 | 3.22 | 14:1 | 36:1 | 944.40 | 184.70 | 0.8 | 1.06 | 5.70 | 6.56 | 795 |
Aerotech C12T | 3.37 | 15:1 | 29:1 | 626.21 | 179.29 | 1.3 | 1.01 | 5.70 | 6.51 | 765 |
Aerotech D13W | 3.76 | 16:1 | 31:1 | 721.18 | 312.86 | 0.9 | 1.75 | 7.20 | 8.75 | 1621 |
Aerotech D10W | 3.51 | 17:1 | 35:1 | 881.12 | 333.93 | 0.9 | 1.44 | 7.30 | 8.54 | 1615 |
Apogee D10 | 3.51 | 19:1 | 35:1 | 885.93 | 337.18 | 0.9 | 1.45 | 7.30 | 8.55 | 1624 |
Aerotech D21T | 3.48 | 29:1 | 44:1 | 1150.48 | 376.59 | 0.7 | 0.95 | 7.60 | 8.35 | 1622 |
Aerotech D24T | 3.69 | 30:1 | 57:1 | 847.94 | 312.89 | 0.9 | 0.95 | 7.40 | 8.15 | 1403 |
Aerotech E25T | 3.31 | 32:1 | 62:1 | 1730.50 | 459.23 | 0.5 | 1.02 | 7.70 | 8.52 | 1849 |
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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