Rocket Motor Guide
Semroc Vector-V
Semroc - Vector-V {Kit} (KV-44)
| 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 | 1.14 | 8:1 | 19:1 | 507.86 | 111.98 | 1.4 | 1.33 | 2.90 | 4.03 | 289 |
| Apogee 1/2A2 | 1.05 | 8:1 | 16:1 | 424.91 | 67.44 | 1.7 | 0.64 | 2.30 | 2.74 | 120 |
| Estes A3T | 1.20 | 9:1 | 23:1 | 587.33 | 102.15 | 1.3 | 1.04 | 2.80 | 3.64 | 235 |
| Estes A10T | 1.09 | 9:1 | 51:1 | 785.61 | 76.80 | 1.1 | 0.91 | 2.40 | 3.11 | 166 |
| Estes 1/4A3T | 1.11 | 9:1 | 20:1 | 492.43 | 20.91 | 1.4 | 0.34 | 1.00 | 1.14 | 16 |
| Apogee 1/4A2 | 1.03 | 10:1 | 22:1 | 590.68 | 24.67 | 1.2 | 0.31 | 1.10 | 1.21 | 21 |
| MPC 1/2A3-M | 1.13 | 12:1 | 20:1 | 423.26 | 56.41 | 1.7 | 0.45 | 2.10 | 2.35 | 85 |
| Estes 1/2A3T | 1.13 | 12:1 | 30:1 | 703.30 | 48.86 | 1.1 | 0.41 | 1.90 | 2.11 | 70 |
| Quest C6 | 1.76 | 13:1 | 62:1 | 1015.53 | 164.28 | 1.7 | 2.57 | 3.70 | 6.07 | 815 |
| Estes A8 | 1.47 | 13:1 | 39:1 | 527.59 | 84.37 | 1.4 | 0.76 | 2.80 | 3.36 | 184 |
| Estes 1/2A6 | 1.39 | 14:1 | 31:1 | 498.54 | 41.70 | 1.6 | 0.37 | 1.70 | 1.87 | 53 |
| Apogee C4 | 1.50 | 15:1 | 45:1 | 829.24 | 190.55 | 1.1 | 2.37 | 3.60 | 5.77 | 805 |
| Estes C5 | 1.64 | 16:1 | 82:1 | 1769.17 | 207.17 | 1.1 | 2.00 | 3.70 | 5.50 | 812 |
| Estes B4 | 1.57 | 17:1 | 51:1 | 786.96 | 142.94 | 1.1 | 1.11 | 3.40 | 4.31 | 379 |
| Weco C6 | 1.64 | 19:1 | 50:1 | 1051.46 | 173.77 | 1.3 | 1.81 | 3.50 | 5.11 | 602 |
| Estes C6 | 1.71 | 19:1 | 56:1 | 749.47 | 215.67 | 1.2 | 1.92 | 3.80 | 5.52 | 764 |
| Estes B6 | 1.54 | 20:1 | 49:1 | 676.67 | 161.59 | 1.2 | 0.92 | 3.50 | 4.22 | 389 |
| Quest A6 | 1.44 | 20:1 | 47:1 | 716.86 | 86.93 | 1.4 | 0.43 | 2.80 | 3.03 | 161 |
| Quest A8 Q-Jet | 1.36 | 20:1 | 45:1 | 937.41 | 95.37 | 1.5 | 0.44 | 2.80 | 3.04 | 171 |
| FSI A6 | 1.47 | 22:1 | 46:1 | 902.62 | 81.69 | 1.3 | 0.51 | 2.50 | 2.81 | 141 |
| Aerotech C6W | 1.71 | 24:1 | 47:1 | 819.62 | 271.31 | 1.3 | 1.71 | 3.80 | 5.31 | 765 |
| Quest B6 | 1.47 | 25:1 | 58:1 | 915.37 | 193.30 | 1.2 | 0.80 | 3.60 | 4.20 | 420 |
| Apogee B7 | 1.22 | 27:1 | 59:1 | 1251.85 | 216.33 | 0.9 | 0.75 | 3.50 | 4.05 | 432 |
| Aerotech D8 | 1.57 | 29:1 | 61:1 | 1314.32 | 377.63 | 0.8 | 2.45 | 3.60 | 5.85 | 1206 |
| Apogee C10 | 1.52 | 40:1 | 103:1 | 2174.46 | 302.30 | 0.6 | 1.04 | 3.90 | 4.74 | 670 |
| Aerotech C12T | 1.67 | 43:1 | 82:1 | 1439.67 | 294.49 | 1.0 | 0.97 | 4.10 | 4.87 | 688 |
| Aerotech D13W | 2.06 | 45:1 | 89:1 | 1466.69 | 397.57 | 0.6 | 1.73 | 4.20 | 5.73 | 1110 |
| Aerotech D10W | 1.81 | 50:1 | 100:1 | 1937.51 | 426.02 | 0.5 | 1.42 | 4.10 | 5.32 | 1049 |
| Apogee D10 | 1.81 | 54:1 | 101:1 | 1949.01 | 430.48 | 0.5 | 1.43 | 4.10 | 5.33 | 1057 |
| Aerotech D21T | 1.78 | 83:1 | 129:1 | 2542.60 | 499.19 | 0.5 | 1.03 | 4.20 | 5.03 | 985 |
| Aerotech D24T | 1.99 | 87:1 | 165:1 | 1510.22 | 415.92 | 0.6 | 0.93 | 4.60 | 5.33 | 950 |
| Aerotech E25T | 1.61 | 93:1 | 178:1 | 3876.45 | 580.86 | 0.4 | 1.01 | 4.00 | 4.81 | 1015 |
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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