Rocket Motor Guide
Dr. Zooch Saturn IB Apollo 5
Dr. Zooch - Saturn IB Apollo 5 {Kit}
| 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 | 3.23 | 2:1 | 6:1 | 146.08 | 31.60 | 12.4 | 1.33 | 1.40 | 2.53 | 61 |
| Estes A3T | 3.30 | 3:1 | 7:1 | 179.77 | 30.74 | 8.2 | 1.09 | 1.30 | 2.19 | 53 |
| Estes A10T | 3.18 | 3:1 | 15:1 | 446.10 | 25.76 | 1.5 | 0.88 | 1.20 | 1.88 | 41 |
| Quest C6 | 3.86 | 4:1 | 19:1 | 449.22 | 94.07 | 2.2 | 2.55 | 3.30 | 5.65 | 440 |
| Estes A8 | 3.58 | 4:1 | 12:1 | 292.21 | 33.41 | 2.1 | 0.74 | 1.50 | 2.04 | 51 |
| Apogee C4 | 3.60 | 5:1 | 14:1 | 337.63 | 99.69 | 2.1 | 2.35 | 3.40 | 5.55 | 474 |
| Estes C5 | 3.74 | 5:1 | 25:1 | 508.39 | 123.52 | 1.5 | 2.05 | 3.70 | 5.55 | 507 |
| Estes B4 | 3.66 | 5:1 | 15:1 | 394.35 | 63.01 | 1.6 | 1.06 | 2.50 | 3.36 | 156 |
| Weco C6 | 3.74 | 6:1 | 15:1 | 349.48 | 81.91 | 1.9 | 1.78 | 3.00 | 4.58 | 284 |
| Estes C6 | 3.81 | 6:1 | 17:1 | 414.96 | 120.61 | 1.7 | 1.88 | 3.80 | 5.48 | 450 |
| Estes B6 | 3.64 | 6:1 | 15:1 | 374.73 | 69.30 | 1.7 | 0.89 | 2.70 | 3.39 | 164 |
| Quest A6 | 3.54 | 6:1 | 14:1 | 362.04 | 29.16 | 1.9 | 0.50 | 1.30 | 1.60 | 33 |
| Quest A8 Q-Jet | 3.46 | 6:1 | 13:1 | 302.36 | 25.31 | 2.2 | 0.44 | 1.20 | 1.44 | 24 |
| FSI A6 | 3.57 | 7:1 | 14:1 | 328.67 | 20.27 | 1.9 | 0.48 | 0.80 | 1.08 | 16 |
| Aerotech C6W | 3.81 | 7:1 | 14:1 | 340.79 | 141.87 | 1.9 | 1.67 | 3.80 | 5.27 | 509 |
| Quest B6 | 3.57 | 7:1 | 17:1 | 416.50 | 77.69 | 1.7 | 0.77 | 2.90 | 3.47 | 183 |
| Apogee B7 | 3.32 | 8:1 | 18:1 | 497.26 | 85.60 | 1.5 | 0.80 | 3.00 | 3.60 | 218 |
| Aerotech D8 | 3.67 | 9:1 | 18:1 | 487.20 | 210.75 | 1.3 | 2.49 | 4.20 | 6.49 | 955 |
| Apogee C10 | 3.62 | 12:1 | 31:1 | 831.36 | 150.03 | 0.9 | 0.96 | 4.10 | 4.86 | 468 |
| Aerotech C12T | 3.77 | 13:1 | 25:1 | 558.02 | 147.03 | 1.3 | 1.01 | 4.10 | 4.91 | 456 |
| Aerotech D13W | 4.16 | 14:1 | 27:1 | 642.50 | 241.80 | 1.0 | 1.75 | 4.60 | 6.15 | 885 |
| Aerotech D10W | 3.91 | 15:1 | 30:1 | 778.94 | 254.22 | 0.9 | 1.45 | 4.80 | 6.05 | 872 |
| Apogee D10 | 3.91 | 16:1 | 30:1 | 783.28 | 255.55 | 1.0 | 1.45 | 4.80 | 6.05 | 874 |
| Aerotech D21T | 3.88 | 25:1 | 39:1 | 1017.29 | 295.16 | 0.7 | 0.95 | 5.10 | 5.85 | 857 |
| Aerotech D24T | 4.09 | 26:1 | 50:1 | 754.15 | 251.04 | 0.9 | 0.96 | 5.10 | 5.86 | 772 |
| Aerotech E25T | 3.71 | 28:1 | 53:1 | 1518.62 | 346.99 | 0.6 | 1.03 | 5.00 | 5.83 | 953 |
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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