Estes HiJinks
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 | 1.76 | 4:1 | 11:1 | 305.58 | 80.03 | 3.4 | 1.33 | 3.10 | 4.23 | 241 |
Apogee 1/2A2 | 1.68 | 5:1 | 9:1 | 250.84 | 41.10 | 3.7 | 0.65 | 1.80 | 2.25 | 67 |
Estes A3T | 1.82 | 5:1 | 14:1 | 363.43 | 70.38 | 1.7 | 1.08 | 2.80 | 3.68 | 191 |
Estes A10T | 1.70 | 6:1 | 30:1 | 670.57 | 44.81 | 1.2 | 0.94 | 1.90 | 2.64 | 95 |
Estes 1/4A3T | 1.74 | 6:1 | 12:1 | 303.22 | 20.15 | 2.2 | 0.29 | 1.00 | 1.09 | 13 |
Apogee 1/4A2 | 1.65 | 6:1 | 13:1 | 353.48 | 20.13 | 2.2 | 0.27 | 1.00 | 1.07 | 13 |
MPC 1/2A3-M | 1.75 | 7:1 | 12:1 | 313.00 | 33.59 | 2.0 | 0.49 | 1.50 | 1.79 | 44 |
Estes 1/2A3T | 1.75 | 7:1 | 18:1 | 491.13 | 31.41 | 1.4 | 0.44 | 1.40 | 1.64 | 39 |
Quest C6 | 2.38 | 7:1 | 37:1 | 724.04 | 181.29 | 1.9 | 2.60 | 5.20 | 7.60 | 1014 |
Estes A8 | 2.10 | 8:1 | 23:1 | 456.45 | 54.95 | 1.6 | 0.79 | 2.40 | 2.99 | 120 |
Estes 1/2A6 | 2.01 | 8:1 | 19:1 | 402.39 | 21.57 | 1.8 | 0.40 | 1.00 | 1.20 | 18 |
Apogee C4 | 2.12 | 9:1 | 27:1 | 591.05 | 191.40 | 1.4 | 2.40 | 5.30 | 7.50 | 1077 |
Estes C5 | 2.26 | 9:1 | 48:1 | 1171.10 | 234.39 | 1.3 | 2.02 | 5.60 | 7.42 | 1124 |
Estes B4 | 2.19 | 10:1 | 30:1 | 661.64 | 112.17 | 1.2 | 1.12 | 4.00 | 4.92 | 375 |
Weco C6 | 2.26 | 11:1 | 29:1 | 495.59 | 168.16 | 1.5 | 1.73 | 4.90 | 6.43 | 724 |
Estes C6 | 2.34 | 11:1 | 33:1 | 569.09 | 220.08 | 1.4 | 1.94 | 5.60 | 7.34 | 991 |
Estes B6 | 2.16 | 12:1 | 29:1 | 532.05 | 122.40 | 1.4 | 0.94 | 4.20 | 4.94 | 402 |
Quest A6 | 2.06 | 12:1 | 28:1 | 467.56 | 54.44 | 1.6 | 0.45 | 2.30 | 2.55 | 100 |
Quest A8 Q-Jet | 1.98 | 12:1 | 26:1 | 621.50 | 63.19 | 1.7 | 0.47 | 2.60 | 2.87 | 128 |
FSI A6 | 2.09 | 13:1 | 27:1 | 528.54 | 56.32 | 1.5 | 0.53 | 2.20 | 2.53 | 99 |
Aerotech C6W | 2.33 | 14:1 | 28:1 | 591.38 | 251.28 | 1.4 | 1.63 | 5.80 | 7.23 | 1093 |
Quest B6 | 2.09 | 15:1 | 34:1 | 533.45 | 143.44 | 1.4 | 0.82 | 4.60 | 5.22 | 474 |
Apogee B7 | 1.84 | 16:1 | 35:1 | 750.28 | 164.25 | 1.2 | 0.77 | 4.70 | 5.27 | 546 |
Aerotech D8 | 2.19 | 17:1 | 36:1 | 895.57 | 380.67 | 0.9 | 2.46 | 6.00 | 8.26 | 1854 |
Apogee C10 | 2.14 | 24:1 | 61:1 | 1479.70 | 267.38 | 0.6 | 1.05 | 5.80 | 6.65 | 1008 |
Aerotech C12T | 2.29 | 25:1 | 49:1 | 990.68 | 260.27 | 1.1 | 0.99 | 6.00 | 6.79 | 995 |
Aerotech D13W | 2.68 | 27:1 | 53:1 | 1068.86 | 408.13 | 0.7 | 1.73 | 6.70 | 8.23 | 1748 |
Aerotech D10W | 2.43 | 30:1 | 59:1 | 1352.97 | 437.29 | 0.6 | 1.43 | 6.70 | 7.93 | 1700 |
Apogee D10 | 2.43 | 32:1 | 59:1 | 1360.41 | 443.32 | 0.7 | 1.43 | 6.70 | 7.93 | 1709 |
Aerotech D21T | 2.40 | 49:1 | 76:1 | 1768.91 | 509.91 | 0.6 | 1.04 | 6.90 | 7.74 | 1672 |
Aerotech D24T | 2.61 | 52:1 | 98:1 | 1226.42 | 422.05 | 0.7 | 0.94 | 7.00 | 7.74 | 1525 |
Aerotech E25T | 2.23 | 55:1 | 105:1 | 2676.12 | 608.77 | 0.5 | 1.02 | 6.70 | 7.52 | 1796 |
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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