Estes Eagle
Estes - Eagle {Kit} (2193) [2005-2008]
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 | 3.44 | 2:1 | 5:1 | 135.33 | 28.54 | 14.2 | 1.34 | 1.30 | 2.44 | 52 |
Estes A3T | 3.50 | 2:1 | 7:1 | 167.20 | 28.79 | 9.5 | 1.06 | 1.30 | 2.16 | 48 |
Estes A10T | 3.38 | 3:1 | 14:1 | 416.71 | 24.49 | 1.6 | 0.88 | 1.10 | 1.78 | 39 |
Quest C6 | 4.06 | 4:1 | 17:1 | 411.83 | 89.76 | 2.3 | 2.56 | 3.30 | 5.66 | 418 |
Estes A8 | 3.77 | 4:1 | 11:1 | 274.54 | 31.92 | 2.3 | 0.75 | 1.40 | 1.95 | 48 |
Apogee C4 | 3.80 | 4:1 | 13:1 | 319.78 | 95.47 | 2.2 | 2.36 | 3.40 | 5.56 | 453 |
Estes C5 | 3.94 | 4:1 | 23:1 | 489.60 | 118.31 | 1.5 | 2.06 | 3.70 | 5.56 | 487 |
Estes B4 | 3.87 | 5:1 | 14:1 | 370.98 | 59.94 | 1.7 | 1.07 | 2.40 | 3.27 | 147 |
Weco C6 | 3.94 | 5:1 | 14:1 | 339.61 | 77.05 | 2.0 | 1.78 | 2.90 | 4.48 | 265 |
Estes C6 | 4.01 | 5:1 | 16:1 | 402.63 | 115.65 | 1.7 | 1.89 | 3.70 | 5.39 | 435 |
Estes B6 | 3.84 | 6:1 | 14:1 | 352.42 | 65.11 | 1.8 | 0.89 | 2.60 | 3.29 | 153 |
Quest A6 | 3.74 | 6:1 | 13:1 | 344.74 | 28.02 | 2.0 | 0.50 | 1.20 | 1.50 | 30 |
Quest A8 Q-Jet | 3.66 | 6:1 | 13:1 | 288.54 | 23.62 | 2.2 | 0.44 | 1.10 | 1.34 | 22 |
FSI A6 | 3.77 | 6:1 | 13:1 | 314.25 | 20.25 | 2.0 | 0.48 | 0.80 | 1.08 | 15 |
Aerotech C6W | 4.01 | 7:1 | 13:1 | 321.25 | 135.68 | 2.0 | 1.68 | 3.80 | 5.28 | 494 |
Quest B6 | 3.77 | 7:1 | 16:1 | 406.06 | 73.20 | 1.8 | 0.77 | 2.80 | 3.37 | 171 |
Apogee B7 | 3.52 | 8:1 | 17:1 | 466.27 | 81.10 | 1.5 | 0.81 | 2.90 | 3.51 | 205 |
Aerotech D8 | 3.87 | 8:1 | 17:1 | 457.96 | 202.73 | 1.4 | 2.50 | 4.30 | 6.60 | 949 |
Apogee C10 | 3.82 | 11:1 | 29:1 | 783.78 | 143.18 | 0.9 | 0.97 | 4.10 | 4.87 | 456 |
Aerotech C12T | 3.97 | 12:1 | 23:1 | 541.79 | 140.19 | 1.3 | 1.02 | 4.10 | 4.92 | 441 |
Aerotech D13W | 4.36 | 13:1 | 25:1 | 608.74 | 234.31 | 1.0 | 1.75 | 4.70 | 6.25 | 881 |
Aerotech D10W | 4.11 | 14:1 | 28:1 | 735.67 | 246.99 | 1.0 | 1.45 | 4.90 | 6.15 | 872 |
Apogee D10 | 4.11 | 15:1 | 28:1 | 739.77 | 247.70 | 1.0 | 1.46 | 4.90 | 6.16 | 872 |
Aerotech D21T | 4.08 | 23:1 | 36:1 | 960.93 | 285.32 | 0.8 | 0.95 | 5.20 | 5.95 | 858 |
Aerotech D24T | 4.29 | 24:1 | 46:1 | 714.24 | 242.49 | 1.0 | 0.96 | 5.10 | 5.86 | 768 |
Aerotech E25T | 3.91 | 26:1 | 50:1 | 1430.23 | 337.09 | 0.6 | 1.03 | 5.10 | 5.93 | 961 |
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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