Rocket Motor Guide
Squirrel Works High 5
| 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 | 1.94 | 4:1 | 10:1 | 272.32 | 69.74 | 4.2 | 1.37 | 2.60 | 3.77 | 188 |
| Apogee 1/2A2 | 1.86 | 4:1 | 8:1 | 222.53 | 37.79 | 4.4 | 0.69 | 1.60 | 2.09 | 58 |
| Estes A3T | 2.00 | 5:1 | 12:1 | 325.48 | 60.59 | 2.0 | 1.09 | 2.40 | 3.29 | 145 |
| Estes A10T | 1.88 | 5:1 | 27:1 | 639.08 | 39.86 | 1.3 | 0.94 | 1.70 | 2.44 | 76 |
| Apogee 1/4A2 | 1.83 | 5:1 | 11:1 | 314.78 | 20.13 | 3.0 | 0.31 | 0.90 | 1.01 | 14 |
| MPC 1/2A3-M | 1.93 | 6:1 | 11:1 | 279.11 | 29.52 | 2.2 | 0.51 | 1.30 | 1.61 | 35 |
| Estes 1/2A3T | 1.93 | 6:1 | 16:1 | 440.25 | 28.33 | 1.4 | 0.44 | 1.30 | 1.54 | 32 |
| Quest C6 | 2.56 | 7:1 | 33:1 | 682.61 | 143.03 | 2.0 | 2.61 | 4.10 | 6.51 | 717 |
| Estes A8 | 2.28 | 7:1 | 21:1 | 436.92 | 49.14 | 1.7 | 0.80 | 2.10 | 2.70 | 97 |
| Estes 1/2A6 | 2.19 | 7:1 | 17:1 | 379.73 | 20.35 | 1.8 | 0.41 | 0.90 | 1.11 | 16 |
| Apogee C4 | 2.30 | 8:1 | 24:1 | 537.09 | 148.65 | 1.5 | 2.40 | 4.10 | 6.30 | 757 |
| Estes C5 | 2.44 | 8:1 | 43:1 | 1045.90 | 185.65 | 1.3 | 2.02 | 4.30 | 6.12 | 781 |
| Estes B4 | 2.37 | 9:1 | 27:1 | 619.07 | 99.03 | 1.2 | 1.13 | 3.30 | 4.23 | 281 |
| Weco C6 | 2.44 | 10:1 | 26:1 | 451.96 | 138.05 | 1.5 | 1.74 | 3.90 | 5.44 | 514 |
| Estes C6 | 2.52 | 10:1 | 30:1 | 543.06 | 180.47 | 1.4 | 1.95 | 4.30 | 6.05 | 691 |
| Estes B6 | 2.34 | 11:1 | 26:1 | 511.97 | 108.72 | 1.5 | 0.95 | 3.50 | 4.25 | 297 |
| Quest A6 | 2.24 | 11:1 | 25:1 | 447.27 | 48.74 | 1.6 | 0.46 | 2.10 | 2.36 | 79 |
| Quest A8 Q-Jet | 2.16 | 11:1 | 24:1 | 508.10 | 54.84 | 1.8 | 0.38 | 2.20 | 2.38 | 87 |
| FSI A6 | 2.27 | 12:1 | 24:1 | 465.73 | 49.08 | 1.5 | 0.54 | 1.90 | 2.24 | 74 |
| Aerotech C6W | 2.51 | 13:1 | 25:1 | 538.16 | 212.99 | 1.5 | 1.63 | 4.50 | 5.93 | 756 |
| Quest B6 | 2.27 | 13:1 | 30:1 | 514.52 | 126.37 | 1.5 | 0.83 | 3.70 | 4.33 | 340 |
| Apogee B7 | 2.02 | 14:1 | 31:1 | 670.72 | 142.73 | 1.2 | 0.78 | 3.80 | 4.38 | 387 |
| Aerotech D8 | 2.37 | 15:1 | 32:1 | 804.39 | 314.08 | 1.0 | 2.47 | 4.50 | 6.77 | 1265 |
| Apogee C10 | 2.32 | 21:1 | 54:1 | 1352.90 | 229.21 | 0.7 | 1.05 | 4.60 | 5.45 | 689 |
| Aerotech C12T | 2.47 | 23:1 | 44:1 | 904.36 | 224.01 | 1.1 | 0.99 | 4.70 | 5.49 | 684 |
| Aerotech D13W | 2.86 | 24:1 | 47:1 | 990.21 | 338.83 | 0.7 | 1.74 | 5.00 | 6.54 | 1175 |
| Aerotech D10W | 2.61 | 26:1 | 53:1 | 1242.93 | 358.89 | 0.7 | 1.43 | 5.10 | 6.33 | 1136 |
| Apogee D10 | 2.61 | 28:1 | 53:1 | 1249.89 | 361.56 | 0.7 | 1.44 | 5.10 | 6.34 | 1141 |
| Aerotech D21T | 2.58 | 44:1 | 68:1 | 1624.32 | 419.35 | 0.6 | 1.04 | 5.20 | 6.04 | 1104 |
| Aerotech D24T | 2.79 | 46:1 | 87:1 | 1169.35 | 354.67 | 0.7 | 0.94 | 5.50 | 6.24 | 1023 |
| Aerotech E25T | 2.41 | 49:1 | 94:1 | 2460.41 | 494.31 | 0.5 | 1.02 | 5.10 | 5.92 | 1180 |
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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