Rocketarium Vortico
Rocketarium - Vortico {Kit} (RK-VORTI)
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 | 0.79 | 12:1 | 32:1 | 680.67 | 33.56 | 1.1 | 1.40 | 0.40 | 1.60 | 56 |
Apogee 1/2A2 | 0.71 | 13:1 | 26:1 | 579.58 | 33.77 | 1.2 | 0.70 | 0.50 | 1.00 | 27 |
Estes A3T | 0.85 | 14:1 | 38:1 | 629.05 | 38.20 | 1.2 | 1.02 | 0.50 | 1.32 | 44 |
Estes A10T | 0.73 | 15:1 | 83:1 | 1287.34 | 108.01 | 1.0 | 0.90 | 0.50 | 1.20 | 19 |
Estes 1/4A3T | 0.77 | 15:1 | 32:1 | 554.40 | 22.63 | 1.3 | 0.32 | 0.50 | 0.62 | 8 |
Apogee 1/4A2 | 0.68 | 16:1 | 35:1 | 753.77 | 30.23 | 1.1 | 0.29 | 0.50 | 0.59 | 8 |
MPC 1/2A3-M | 0.78 | 20:1 | 33:1 | 467.38 | 52.21 | 1.5 | 0.53 | 0.40 | 0.73 | 17 |
Estes 1/2A3T | 0.78 | 20:1 | 50:1 | 733.32 | 43.18 | 1.0 | 0.40 | 0.50 | 0.70 | 15 |
Quest C6 | 1.41 | 21:1 | 101:1 | 1026.15 | 97.48 | 1.7 | 2.55 | 0.70 | 3.05 | 144 |
Estes A8 | 1.13 | 21:1 | 64:1 | 693.68 | 67.66 | 1.4 | 0.75 | 0.60 | 1.15 | 37 |
Estes 1/2A6 | 1.04 | 22:1 | 51:1 | 577.86 | 59.84 | 1.5 | 0.35 | 0.40 | 0.55 | 12 |
Apogee C4 | 1.15 | 25:1 | 74:1 | 931.30 | 92.74 | 0.9 | 2.36 | 0.60 | 2.76 | 143 |
Estes C5 | 1.29 | 26:1 | 134:1 | 2254.34 | 173.88 | 1.0 | 2.09 | 0.50 | 2.39 | 111 |
Estes B4 | 1.22 | 27:1 | 83:1 | 841.29 | 70.96 | 1.0 | 1.10 | 0.60 | 1.50 | 66 |
Weco C6 | 1.29 | 31:1 | 81:1 | 1393.58 | 115.29 | 1.1 | -1.00 | 1.39 | 0.19 | 12 |
Estes C6 | 1.37 | 31:1 | 92:1 | 1234.75 | 104.33 | 1.2 | -1.00 | 1.41 | 0.21 | 16 |
Estes B6 | 1.19 | 33:1 | 79:1 | 963.06 | 85.85 | 1.2 | 0.91 | 0.60 | 1.31 | 59 |
Quest A6 | 1.09 | 33:1 | 77:1 | 1142.77 | 98.37 | 1.3 | 0.41 | 0.10 | 0.31 | 15 |
Quest A8 Q-Jet | 1.01 | 33:1 | 73:1 | 1152.85 | 99.08 | 1.4 | -1.00 | 1.42 | 0.22 | 12 |
FSI A6 | 1.12 | 36:1 | 75:1 | 1181.64 | 101.13 | 1.2 | -1.00 | 1.40 | 0.20 | 11 |
Aerotech C6W | 1.36 | 39:1 | 77:1 | 966.50 | 86.13 | 1.2 | 1.69 | 0.50 | 1.99 | 125 |
Quest B6 | 1.12 | 41:1 | 94:1 | 1581.54 | 128.12 | 1.1 | -1.00 | 1.39 | 0.19 | 11 |
Apogee B7 | 0.87 | 44:1 | 97:1 | 1746.07 | 139.39 | 0.8 | -1.00 | 1.34 | 0.14 | 8 |
Aerotech D8 | 1.22 | 47:1 | 100:1 | 1739.25 | 139.62 | 0.7 | -1.00 | 1.34 | 0.14 | 18 |
Apogee C10 | 1.17 | 65:1 | 168:1 | 2503.91 | 155.78 | 0.5 | -1.00 | 1.33 | 0.13 | 17 |
Aerotech C12T | 1.32 | 70:1 | 135:1 | 1837.28 | 145.85 | 0.9 | 0.96 | 0.70 | 1.46 | 87 |
Aerotech D13W | 1.71 | 74:1 | 146:1 | 1844.90 | 142.54 | 0.5 | 1.72 | 0.60 | 2.12 | 171 |
Aerotech D10W | 1.46 | 82:1 | 164:1 | 2452.79 | 158.97 | 0.5 | -1.00 | 1.72 | 0.52 | 72 |
Apogee D10 | 1.46 | 88:1 | 164:1 | 2534.48 | 162.35 | 0.5 | -1.00 | 1.72 | 0.52 | 73 |
Aerotech D21T | 1.43 | 136:1 | 210:1 | 3131.86 | 233.10 | 0.5 | -1.00 | 1.33 | 0.13 | 4 |
Aerotech D24T | 1.64 | 142:1 | 270:1 | 1839.91 | 146.98 | 0.6 | 0.93 | 0.70 | 1.43 | 120 |
Aerotech E25T | 1.26 | 152:1 | 291:1 | 5234.89 | 342.11 | 0.4 | -1.00 | 1.91 | 0.11 | 5 |
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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