Estes Nike Apache
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 | 2.04 | 4:1 | 10:1 | 256.76 | 62.35 | 4.6 | 1.40 | 2.40 | 3.60 | 165 |
Apogee 1/2A2 | 1.95 | 4:1 | 8:1 | 209.33 | 31.92 | 4.8 | 0.71 | 1.40 | 1.91 | 47 |
Estes A3T | 2.10 | 4:1 | 12:1 | 307.72 | 58.08 | 2.1 | 1.10 | 2.30 | 3.20 | 135 |
Estes A10T | 1.98 | 5:1 | 25:1 | 627.62 | 38.13 | 1.3 | 0.94 | 1.60 | 2.34 | 71 |
MPC 1/2A3-M | 2.03 | 6:1 | 10:1 | 263.48 | 28.03 | 2.3 | 0.52 | 1.30 | 1.62 | 32 |
Estes 1/2A3T | 2.03 | 6:1 | 15:1 | 416.57 | 27.00 | 1.5 | 0.45 | 1.20 | 1.45 | 30 |
Quest C6 | 2.66 | 6:1 | 31:1 | 661.55 | 139.40 | 2.0 | 2.61 | 4.00 | 6.41 | 698 |
Estes A8 | 2.37 | 6:1 | 19:1 | 424.11 | 47.16 | 1.7 | 0.80 | 2.00 | 2.60 | 90 |
Estes 1/2A6 | 2.29 | 7:1 | 16:1 | 366.46 | 20.26 | 1.9 | 0.41 | 0.90 | 1.11 | 15 |
Apogee C4 | 2.40 | 8:1 | 23:1 | 514.55 | 145.82 | 1.5 | 2.41 | 4.10 | 6.31 | 743 |
Estes C5 | 2.54 | 8:1 | 41:1 | 982.49 | 181.45 | 1.3 | 2.03 | 4.30 | 6.13 | 769 |
Estes B4 | 2.47 | 8:1 | 26:1 | 601.78 | 95.37 | 1.3 | 1.03 | 3.30 | 4.13 | 269 |
Weco C6 | 2.54 | 9:1 | 25:1 | 442.61 | 132.98 | 1.6 | 1.74 | 3.90 | 5.44 | 496 |
Estes C6 | 2.61 | 9:1 | 28:1 | 530.04 | 175.81 | 1.4 | 1.95 | 4.30 | 6.05 | 678 |
Estes B6 | 2.44 | 10:1 | 24:1 | 502.97 | 104.25 | 1.5 | 0.95 | 3.40 | 4.15 | 284 |
Quest A6 | 2.34 | 10:1 | 24:1 | 440.49 | 46.24 | 1.7 | 0.46 | 2.00 | 2.26 | 73 |
Quest A8 Q-Jet | 2.26 | 10:1 | 22:1 | 443.29 | 50.59 | 1.8 | 0.39 | 2.10 | 2.29 | 77 |
FSI A6 | 2.37 | 11:1 | 23:1 | 453.21 | 45.72 | 1.5 | 0.54 | 1.80 | 2.14 | 66 |
Aerotech C6W | 2.61 | 12:1 | 24:1 | 515.58 | 206.57 | 1.5 | 1.63 | 4.50 | 5.93 | 746 |
Quest B6 | 2.37 | 12:1 | 29:1 | 503.89 | 120.70 | 1.5 | 0.83 | 3.70 | 4.33 | 326 |
Apogee B7 | 2.12 | 13:1 | 30:1 | 640.49 | 136.70 | 1.3 | 0.78 | 3.80 | 4.38 | 376 |
Aerotech D8 | 2.47 | 14:1 | 31:1 | 767.23 | 305.62 | 1.0 | 2.47 | 4.60 | 6.87 | 1262 |
Apogee C10 | 2.42 | 20:1 | 51:1 | 1292.07 | 221.77 | 0.7 | 1.05 | 4.60 | 5.45 | 682 |
Aerotech C12T | 2.57 | 22:1 | 41:1 | 863.13 | 216.77 | 1.1 | 0.99 | 4.70 | 5.49 | 675 |
Aerotech D13W | 2.96 | 23:1 | 45:1 | 951.63 | 331.23 | 0.7 | 1.74 | 5.10 | 6.64 | 1172 |
Aerotech D10W | 2.71 | 25:1 | 50:1 | 1189.76 | 350.73 | 0.7 | 1.43 | 5.10 | 6.33 | 1135 |
Apogee D10 | 2.71 | 27:1 | 50:1 | 1196.40 | 353.42 | 0.7 | 1.44 | 5.10 | 6.34 | 1140 |
Aerotech D21T | 2.68 | 42:1 | 64:1 | 1554.51 | 409.44 | 0.6 | 1.04 | 5.30 | 6.14 | 1107 |
Aerotech D24T | 2.89 | 44:1 | 83:1 | 1122.99 | 346.71 | 0.7 | 0.94 | 5.50 | 6.24 | 1021 |
Aerotech E25T | 2.51 | 47:1 | 89:1 | 2344.62 | 484.00 | 0.5 | 1.02 | 5.20 | 6.02 | 1188 |
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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