Dr. Zooch Mark II
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 | 2.63 | 3:1 | 7:1 | 188.36 | 46.98 | 7.5 | 1.36 | 2.10 | 3.26 | 113 |
Apogee 1/2A2 | 2.55 | 3:1 | 6:1 | 151.52 | 23.91 | 7.5 | 0.68 | 1.10 | 1.58 | 28 |
Estes A3T | 2.70 | 3:1 | 9:1 | 229.05 | 43.42 | 4.5 | 1.01 | 2.00 | 2.81 | 90 |
Estes A10T | 2.58 | 4:1 | 19:1 | 536.26 | 30.91 | 1.4 | 0.86 | 1.40 | 2.06 | 53 |
MPC 1/2A3-M | 2.63 | 5:1 | 8:1 | 194.53 | 21.64 | 3.8 | 0.50 | 1.00 | 1.30 | 20 |
Estes 1/2A3T | 2.63 | 5:1 | 11:1 | 312.00 | 24.44 | 2.5 | 0.40 | 1.10 | 1.30 | 24 |
Quest C6 | 3.26 | 5:1 | 23:1 | 563.54 | 136.91 | 2.1 | 2.63 | 4.80 | 7.23 | 761 |
Estes A8 | 2.98 | 5:1 | 15:1 | 355.73 | 39.40 | 1.9 | 0.82 | 1.70 | 2.32 | 69 |
Estes 1/2A6 | 2.89 | 5:1 | 12:1 | 292.90 | 20.15 | 2.1 | 0.34 | 1.00 | 1.14 | 13 |
Apogee C4 | 3.00 | 6:1 | 17:1 | 412.42 | 148.48 | 1.8 | 2.43 | 5.10 | 7.33 | 842 |
Estes C5 | 3.14 | 6:1 | 31:1 | 697.18 | 177.86 | 1.4 | 2.04 | 5.60 | 7.44 | 917 |
Estes B4 | 3.07 | 6:1 | 19:1 | 484.39 | 79.05 | 1.4 | 1.05 | 3.30 | 4.15 | 238 |
Weco C6 | 3.14 | 7:1 | 19:1 | 389.40 | 115.50 | 1.8 | 1.76 | 4.30 | 5.86 | 491 |
Estes C6 | 3.21 | 7:1 | 21:1 | 462.72 | 164.25 | 1.6 | 1.87 | 5.40 | 7.07 | 776 |
Estes B6 | 3.04 | 8:1 | 18:1 | 453.44 | 85.77 | 1.6 | 0.87 | 3.50 | 4.17 | 254 |
Quest A6 | 2.94 | 8:1 | 18:1 | 395.53 | 35.18 | 1.8 | 0.48 | 1.60 | 1.88 | 49 |
Quest A8 Q-Jet | 2.86 | 8:1 | 17:1 | 333.74 | 32.64 | 2.0 | 0.41 | 1.50 | 1.71 | 38 |
FSI A6 | 2.97 | 8:1 | 17:1 | 383.70 | 24.96 | 1.7 | 0.56 | 1.00 | 1.36 | 24 |
Aerotech C6W | 3.21 | 9:1 | 18:1 | 415.40 | 189.28 | 1.7 | 1.65 | 5.70 | 7.15 | 917 |
Quest B6 | 2.97 | 9:1 | 22:1 | 453.53 | 98.00 | 1.6 | 0.85 | 3.80 | 4.45 | 297 |
Apogee B7 | 2.72 | 10:1 | 22:1 | 618.92 | 112.20 | 1.3 | 0.79 | 4.20 | 4.79 | 378 |
Aerotech D8 | 3.07 | 11:1 | 23:1 | 604.31 | 302.99 | 1.1 | 2.48 | 6.80 | 9.08 | 1813 |
Apogee C10 | 3.02 | 15:1 | 39:1 | 1013.37 | 197.20 | 0.8 | 1.06 | 5.90 | 6.76 | 852 |
Aerotech C12T | 3.17 | 16:1 | 31:1 | 673.62 | 191.28 | 1.2 | 1.00 | 5.90 | 6.70 | 820 |
Aerotech D13W | 3.56 | 17:1 | 33:1 | 768.26 | 329.33 | 0.9 | 1.74 | 7.20 | 8.74 | 1687 |
Aerotech D10W | 3.31 | 19:1 | 38:1 | 943.00 | 351.66 | 0.8 | 1.44 | 7.30 | 8.54 | 1673 |
Apogee D10 | 3.31 | 20:1 | 38:1 | 948.15 | 355.83 | 0.8 | 1.44 | 7.40 | 8.64 | 1684 |
Aerotech D21T | 3.28 | 31:1 | 48:1 | 1231.30 | 398.81 | 0.6 | 0.94 | 7.70 | 8.44 | 1679 |
Aerotech D24T | 3.49 | 33:1 | 62:1 | 904.02 | 330.41 | 0.8 | 0.95 | 7.50 | 8.25 | 1461 |
Aerotech E25T | 3.11 | 35:1 | 67:1 | 1860.58 | 486.06 | 0.5 | 1.02 | 7.70 | 8.52 | 1897 |
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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