Estes Aries SST
Estes - Aries SST {Kit} (1927) [1984-1985]
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 | 1.58 | 5:1 | 13:1 | 346.82 | 89.08 | 2.8 | 1.40 | 3.30 | 4.50 | 281 |
Apogee 1/2A2 | 1.50 | 5:1 | 11:1 | 286.06 | 47.12 | 3.0 | 0.71 | 2.00 | 2.51 | 88 |
Estes A3T | 1.64 | 6:1 | 16:1 | 409.99 | 80.48 | 1.5 | 1.06 | 3.10 | 3.96 | 225 |
Estes A10T | 1.52 | 6:1 | 34:1 | 698.23 | 50.54 | 1.2 | 0.93 | 2.20 | 2.93 | 112 |
Estes 1/4A3T | 1.56 | 6:1 | 13:1 | 342.62 | 20.25 | 1.8 | 0.27 | 1.00 | 1.07 | 13 |
Apogee 1/4A2 | 1.47 | 7:1 | 15:1 | 401.56 | 20.26 | 1.8 | 0.25 | 1.00 | 1.05 | 13 |
MPC 1/2A3-M | 1.57 | 8:1 | 13:1 | 354.30 | 38.11 | 1.9 | 0.48 | 1.70 | 1.98 | 54 |
Estes 1/2A3T | 1.57 | 8:1 | 20:1 | 553.51 | 34.79 | 1.3 | 0.43 | 1.60 | 1.83 | 46 |
Quest C6 | 2.20 | 8:1 | 42:1 | 772.99 | 192.94 | 1.9 | 2.59 | 5.30 | 7.69 | 1076 |
Estes A8 | 1.92 | 9:1 | 26:1 | 474.43 | 61.15 | 1.6 | 0.78 | 2.60 | 3.18 | 140 |
Estes 1/2A6 | 1.83 | 9:1 | 21:1 | 424.13 | 25.09 | 1.7 | 0.39 | 1.20 | 1.39 | 23 |
Apogee C4 | 1.94 | 10:1 | 30:1 | 647.75 | 200.69 | 1.3 | 2.39 | 5.30 | 7.49 | 1118 |
Estes C5 | 2.08 | 11:1 | 55:1 | 1334.21 | 247.79 | 1.2 | 2.01 | 5.50 | 7.31 | 1163 |
Estes B4 | 2.01 | 11:1 | 34:1 | 707.98 | 122.62 | 1.1 | 1.12 | 4.10 | 5.02 | 418 |
Weco C6 | 2.08 | 13:1 | 33:1 | 613.19 | 182.73 | 1.4 | 1.72 | 5.00 | 6.52 | 775 |
Estes C6 | 2.16 | 13:1 | 38:1 | 600.69 | 235.14 | 1.3 | 1.94 | 5.50 | 7.24 | 1037 |
Estes B6 | 1.98 | 14:1 | 33:1 | 556.50 | 134.40 | 1.4 | 0.94 | 4.40 | 5.14 | 445 |
Quest A6 | 1.88 | 14:1 | 32:1 | 486.47 | 61.08 | 1.6 | 0.44 | 2.60 | 2.84 | 120 |
Quest A8 Q-Jet | 1.80 | 14:1 | 30:1 | 752.32 | 74.76 | 1.7 | 0.47 | 3.00 | 3.27 | 164 |
FSI A6 | 1.91 | 15:1 | 31:1 | 620.28 | 62.67 | 1.4 | 0.53 | 2.40 | 2.73 | 118 |
Aerotech C6W | 2.15 | 16:1 | 32:1 | 647.05 | 268.37 | 1.4 | 1.62 | 5.70 | 7.12 | 1122 |
Quest B6 | 1.91 | 17:1 | 39:1 | 562.92 | 159.66 | 1.4 | 0.82 | 4.70 | 5.32 | 520 |
Apogee B7 | 1.66 | 18:1 | 40:1 | 856.67 | 182.01 | 1.1 | 0.76 | 4.80 | 5.36 | 586 |
Aerotech D8 | 2.01 | 19:1 | 41:1 | 991.42 | 406.18 | 0.9 | 2.46 | 5.80 | 8.06 | 1854 |
Apogee C10 | 1.96 | 27:1 | 69:1 | 1631.68 | 287.31 | 0.6 | 1.04 | 5.80 | 6.64 | 1030 |
Aerotech C12T | 2.11 | 29:1 | 55:1 | 1091.37 | 279.54 | 1.0 | 0.98 | 6.00 | 6.78 | 1025 |
Aerotech D13W | 2.50 | 30:1 | 60:1 | 1160.61 | 428.66 | 0.7 | 1.73 | 6.50 | 8.03 | 1754 |
Aerotech D10W | 2.25 | 34:1 | 67:1 | 1483.47 | 459.48 | 0.6 | 1.43 | 6.50 | 7.73 | 1696 |
Apogee D10 | 2.25 | 36:1 | 67:1 | 1491.65 | 466.81 | 0.6 | 1.43 | 6.50 | 7.73 | 1709 |
Aerotech D21T | 2.22 | 56:1 | 86:1 | 1940.85 | 537.36 | 0.5 | 1.03 | 6.60 | 7.43 | 1659 |
Aerotech D24T | 2.43 | 58:1 | 111:1 | 1291.96 | 445.83 | 0.7 | 0.94 | 6.90 | 7.64 | 1530 |
Aerotech E25T | 2.05 | 62:1 | 120:1 | 2936.77 | 643.01 | 0.5 | 1.02 | 6.40 | 7.22 | 1762 |
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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