Rocket Motor Guide
Semroc Jupiter B
Semroc - Jupiter B {Kit} (KN-06) [2019-]
| 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 | 1.26 | 7:1 | 17:1 | 434.40 | 32.89 | 2.1 | 1.36 | 0.70 | 1.86 | 60 |
| Apogee 1/2A2 | 1.17 | 7:1 | 14:1 | 359.17 | 32.85 | 2.5 | 0.67 | 0.70 | 1.17 | 28 |
| Estes A3T | 1.32 | 8:1 | 21:1 | 486.73 | 34.36 | 1.4 | 1.05 | 0.70 | 1.55 | 48 |
| Estes A10T | 1.21 | 8:1 | 45:1 | 712.88 | 29.65 | 1.2 | 0.92 | 0.60 | 1.32 | 34 |
| Estes 1/4A3T | 1.23 | 8:1 | 17:1 | 405.43 | 20.27 | 1.6 | 0.35 | 0.50 | 0.65 | 7 |
| Apogee 1/4A2 | 1.15 | 9:1 | 19:1 | 489.57 | 20.18 | 1.4 | 0.32 | 0.60 | 0.72 | 7 |
| MPC 1/2A3-M | 1.25 | 11:1 | 18:1 | 357.29 | 35.85 | 1.8 | 0.46 | 0.70 | 0.96 | 20 |
| Estes 1/2A3T | 1.25 | 11:1 | 27:1 | 604.82 | 31.44 | 1.2 | 0.42 | 0.70 | 0.92 | 18 |
| Quest C6 | 1.88 | 11:1 | 55:1 | 840.29 | 96.39 | 1.8 | 2.58 | 0.80 | 3.18 | 158 |
| Estes A8 | 1.59 | 11:1 | 34:1 | 479.89 | 38.92 | 1.5 | 0.77 | 0.80 | 1.37 | 38 |
| Estes 1/2A6 | 1.51 | 12:1 | 28:1 | 437.44 | 31.62 | 1.6 | 0.38 | 0.80 | 0.98 | 15 |
| Apogee C4 | 1.62 | 13:1 | 40:1 | 648.09 | 85.99 | 1.1 | 2.38 | 0.80 | 2.98 | 156 |
| Estes C5 | 1.76 | 14:1 | 72:1 | 1599.45 | 129.19 | 1.1 | 2.01 | 0.80 | 2.61 | 145 |
| Estes B4 | 1.69 | 15:1 | 45:1 | 726.97 | 47.30 | 1.1 | 1.11 | 0.80 | 1.71 | 69 |
| Weco C6 | 1.76 | 17:1 | 44:1 | 831.99 | 77.19 | 1.4 | 1.71 | 0.80 | 2.31 | 112 |
| Estes C6 | 1.83 | 17:1 | 50:1 | 616.67 | 58.08 | 1.3 | 1.93 | 0.90 | 2.63 | 144 |
| Estes B6 | 1.66 | 18:1 | 43:1 | 575.44 | 57.59 | 1.3 | 0.93 | 0.80 | 1.53 | 65 |
| Quest A6 | 1.56 | 18:1 | 42:1 | 549.21 | 57.64 | 1.5 | 0.43 | 0.80 | 1.03 | 29 |
| Quest A8 Q-Jet | 1.48 | 18:1 | 39:1 | 845.55 | 77.87 | 1.6 | 0.45 | 0.70 | 0.95 | 26 |
| FSI A6 | 1.59 | 19:1 | 40:1 | 754.69 | 71.91 | 1.3 | 0.52 | 0.70 | 1.02 | 25 |
| Aerotech C6W | 1.83 | 21:1 | 42:1 | 706.21 | 89.60 | 1.3 | 1.61 | 0.80 | 2.21 | 133 |
| Quest B6 | 1.59 | 22:1 | 51:1 | 729.12 | 70.17 | 1.3 | 0.81 | 0.80 | 1.41 | 65 |
| Apogee B7 | 1.34 | 24:1 | 52:1 | 1072.43 | 93.33 | 1.0 | 0.75 | 0.70 | 1.25 | 64 |
| Aerotech D8 | 1.69 | 25:1 | 54:1 | 1147.60 | 101.32 | 0.8 | 2.45 | 0.70 | 2.95 | 236 |
| Apogee C10 | 1.64 | 35:1 | 91:1 | 1964.39 | 111.30 | 0.6 | 1.04 | 0.80 | 1.64 | 105 |
| Aerotech C12T | 1.79 | 38:1 | 73:1 | 1281.95 | 108.05 | 1.0 | 0.98 | 0.90 | 1.68 | 105 |
| Aerotech D13W | 2.18 | 40:1 | 79:1 | 1367.43 | 125.38 | 0.6 | 1.73 | 0.80 | 2.33 | 191 |
| Aerotech D10W | 1.93 | 44:1 | 88:1 | 1763.01 | 118.42 | 0.5 | 1.42 | 0.80 | 2.02 | 181 |
| Apogee D10 | 1.93 | 47:1 | 89:1 | 1789.66 | 121.27 | 0.5 | 1.43 | 0.80 | 2.03 | 182 |
| Aerotech D21T | 1.90 | 74:1 | 113:1 | 2322.06 | 167.97 | 0.5 | 1.03 | 0.80 | 1.63 | 150 |
| Aerotech D24T | 2.11 | 77:1 | 146:1 | 1419.63 | 120.42 | 0.7 | 0.93 | 1.00 | 1.73 | 145 |
| Aerotech E25T | 1.73 | 82:1 | 157:1 | 3519.74 | 229.80 | 0.4 | -1.00 | 1.31 | 0.11 | 31 |
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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