Quest The Flash
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 | 1.84 | 4:1 | 11:1 | 289.82 | 78.56 | 3.7 | 1.35 | 3.30 | 4.45 | 249 |
Apogee 1/2A2 | 1.76 | 4:1 | 9:1 | 237.43 | 39.98 | 4.0 | 0.67 | 1.80 | 2.27 | 66 |
Estes A3T | 1.90 | 5:1 | 13:1 | 345.62 | 67.59 | 1.8 | 1.08 | 2.90 | 3.78 | 189 |
Estes A10T | 1.78 | 5:1 | 28:1 | 654.04 | 43.21 | 1.2 | 0.94 | 1.90 | 2.64 | 92 |
Estes 1/4A3T | 1.82 | 5:1 | 11:1 | 288.15 | 20.18 | 2.5 | 0.30 | 1.00 | 1.10 | 14 |
Apogee 1/4A2 | 1.73 | 6:1 | 12:1 | 335.22 | 20.20 | 2.4 | 0.28 | 1.00 | 1.08 | 14 |
MPC 1/2A3-M | 1.83 | 7:1 | 11:1 | 297.40 | 31.90 | 2.1 | 0.50 | 1.50 | 1.80 | 41 |
Estes 1/2A3T | 1.83 | 7:1 | 17:1 | 467.39 | 30.13 | 1.4 | 0.44 | 1.40 | 1.64 | 37 |
Quest C6 | 2.46 | 7:1 | 35:1 | 706.20 | 194.47 | 1.9 | 2.60 | 6.20 | 8.60 | 1203 |
Estes A8 | 2.18 | 7:1 | 22:1 | 449.37 | 52.96 | 1.6 | 0.79 | 2.40 | 2.99 | 117 |
Estes 1/2A6 | 2.09 | 8:1 | 18:1 | 390.91 | 20.70 | 1.8 | 0.40 | 1.00 | 1.20 | 17 |
Apogee C4 | 2.20 | 9:1 | 25:1 | 571.03 | 210.75 | 1.4 | 2.40 | 6.30 | 8.50 | 1313 |
Estes C5 | 2.35 | 9:1 | 46:1 | 1111.59 | 252.45 | 1.3 | 2.02 | 6.70 | 8.52 | 1396 |
Estes B4 | 2.27 | 9:1 | 29:1 | 643.06 | 110.01 | 1.2 | 1.13 | 4.20 | 5.13 | 399 |
Weco C6 | 2.34 | 11:1 | 28:1 | 467.58 | 172.23 | 1.5 | 1.73 | 5.70 | 7.23 | 838 |
Estes C6 | 2.42 | 11:1 | 32:1 | 559.11 | 229.54 | 1.4 | 1.95 | 6.50 | 8.25 | 1201 |
Estes B6 | 2.24 | 11:1 | 27:1 | 519.11 | 119.48 | 1.4 | 0.95 | 4.50 | 5.25 | 434 |
Quest A6 | 2.14 | 11:1 | 27:1 | 459.88 | 52.06 | 1.6 | 0.45 | 2.30 | 2.55 | 96 |
Quest A8 Q-Jet | 2.06 | 11:1 | 25:1 | 565.44 | 58.92 | 1.8 | 0.48 | 2.50 | 2.78 | 115 |
FSI A6 | 2.17 | 12:1 | 26:1 | 481.16 | 52.82 | 1.5 | 0.53 | 2.10 | 2.43 | 92 |
Aerotech C6W | 2.41 | 13:1 | 26:1 | 571.86 | 259.57 | 1.5 | 1.63 | 6.90 | 8.33 | 1361 |
Quest B6 | 2.17 | 14:1 | 32:1 | 526.87 | 140.06 | 1.4 | 0.83 | 5.00 | 5.63 | 526 |
Apogee B7 | 1.92 | 15:1 | 33:1 | 713.37 | 161.42 | 1.2 | 0.77 | 5.30 | 5.87 | 632 |
Aerotech D8 | 2.27 | 16:1 | 35:1 | 863.41 | 408.63 | 0.9 | 2.46 | 7.60 | 9.86 | 2460 |
Apogee C10 | 2.22 | 22:1 | 58:1 | 1420.00 | 272.74 | 0.6 | 1.05 | 7.00 | 7.85 | 1270 |
Aerotech C12T | 2.37 | 24:1 | 46:1 | 950.42 | 263.94 | 1.1 | 0.99 | 7.10 | 7.89 | 1235 |
Aerotech D13W | 2.77 | 25:1 | 50:1 | 1031.96 | 434.53 | 0.7 | 1.73 | 8.30 | 9.83 | 2314 |
Aerotech D10W | 2.52 | 28:1 | 56:1 | 1301.31 | 470.96 | 0.6 | 1.43 | 8.30 | 9.53 | 2277 |
Apogee D10 | 2.52 | 30:1 | 56:1 | 1308.38 | 477.24 | 0.7 | 1.43 | 8.30 | 9.53 | 2292 |
Aerotech D21T | 2.48 | 47:1 | 72:1 | 1700.90 | 537.43 | 0.6 | 1.04 | 8.50 | 9.34 | 2270 |
Aerotech D24T | 2.69 | 49:1 | 93:1 | 1202.04 | 437.90 | 0.7 | 0.94 | 8.60 | 9.34 | 2012 |
Aerotech E25T | 2.31 | 52:1 | 100:1 | 2562.46 | 660.55 | 0.5 | 1.02 | 8.50 | 9.32 | 2492 |
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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