Estes Recruiter
Estes - Recruiter {Kit} (2013)
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 | 2.81 | 3:1 | 7:1 | 173.67 | 39.81 | 8.8 | 1.34 | 1.70 | 2.84 | 84 |
Apogee 1/2A2 | 2.73 | 3:1 | 6:1 | 139.16 | 20.16 | 8.6 | 0.64 | 0.90 | 1.34 | 20 |
Estes A3T | 2.88 | 3:1 | 8:1 | 211.91 | 39.07 | 5.6 | 1.06 | 1.70 | 2.56 | 75 |
Estes A10T | 2.77 | 3:1 | 18:1 | 514.44 | 28.62 | 1.4 | 0.86 | 1.30 | 1.96 | 47 |
MPC 1/2A3-M | 2.81 | 4:1 | 7:1 | 179.33 | 20.14 | 4.5 | 0.43 | 0.90 | 1.13 | 16 |
Estes 1/2A3T | 2.81 | 4:1 | 11:1 | 289.15 | 21.60 | 3.2 | 0.43 | 1.00 | 1.23 | 19 |
Quest C6 | 3.44 | 4:1 | 22:1 | 532.67 | 103.42 | 2.1 | 2.64 | 3.30 | 5.74 | 487 |
Estes A8 | 3.15 | 4:1 | 14:1 | 336.51 | 36.89 | 1.9 | 0.83 | 1.50 | 2.13 | 59 |
Estes 1/2A6 | 3.07 | 5:1 | 11:1 | 272.51 | 20.18 | 2.2 | 0.35 | 0.90 | 1.05 | 14 |
Apogee C4 | 3.18 | 5:1 | 16:1 | 382.55 | 108.52 | 1.9 | 2.44 | 3.40 | 5.64 | 521 |
Estes C5 | 3.32 | 5:1 | 28:1 | 631.08 | 135.36 | 1.4 | 2.05 | 3.70 | 5.55 | 549 |
Estes B4 | 3.25 | 6:1 | 18:1 | 453.06 | 70.97 | 1.4 | 1.05 | 2.70 | 3.55 | 180 |
Weco C6 | 3.32 | 7:1 | 17:1 | 376.07 | 94.33 | 1.8 | 1.77 | 3.20 | 4.77 | 328 |
Estes C6 | 3.39 | 7:1 | 20:1 | 446.90 | 132.28 | 1.6 | 1.87 | 3.80 | 5.47 | 484 |
Estes B6 | 3.22 | 7:1 | 17:1 | 430.76 | 77.87 | 1.6 | 0.87 | 2.90 | 3.57 | 188 |
Quest A6 | 3.12 | 7:1 | 16:1 | 384.83 | 32.43 | 1.9 | 0.49 | 1.50 | 1.79 | 41 |
Quest A8 Q-Jet | 3.04 | 7:1 | 16:1 | 320.16 | 29.78 | 2.1 | 0.42 | 1.30 | 1.52 | 32 |
FSI A6 | 3.15 | 8:1 | 16:1 | 364.37 | 22.57 | 1.8 | 0.47 | 1.00 | 1.27 | 19 |
Aerotech C6W | 3.39 | 8:1 | 16:1 | 389.19 | 156.42 | 1.8 | 1.66 | 3.90 | 5.36 | 542 |
Quest B6 | 3.15 | 9:1 | 20:1 | 440.60 | 88.93 | 1.6 | 0.75 | 3.10 | 3.65 | 211 |
Apogee B7 | 2.90 | 9:1 | 21:1 | 576.20 | 98.54 | 1.4 | 0.79 | 3.20 | 3.79 | 251 |
Aerotech D8 | 3.25 | 10:1 | 21:1 | 558.83 | 230.24 | 1.2 | 2.49 | 4.10 | 6.39 | 971 |
Apogee C10 | 3.20 | 14:1 | 36:1 | 951.05 | 166.80 | 0.8 | 1.06 | 4.00 | 4.86 | 496 |
Aerotech C12T | 3.35 | 15:1 | 29:1 | 629.39 | 163.49 | 1.3 | 1.01 | 4.10 | 4.91 | 487 |
Aerotech D13W | 3.74 | 16:1 | 31:1 | 725.86 | 258.86 | 0.9 | 1.75 | 4.50 | 6.05 | 896 |
Aerotech D10W | 3.49 | 17:1 | 35:1 | 887.08 | 272.32 | 0.8 | 1.44 | 4.60 | 5.84 | 876 |
Apogee D10 | 3.49 | 19:1 | 35:1 | 892.04 | 274.13 | 0.9 | 1.45 | 4.60 | 5.85 | 880 |
Aerotech D21T | 3.46 | 29:1 | 45:1 | 1158.34 | 317.53 | 0.7 | 0.95 | 4.90 | 5.65 | 858 |
Aerotech D24T | 3.67 | 30:1 | 58:1 | 852.98 | 270.75 | 0.9 | 0.95 | 4.90 | 5.65 | 782 |
Aerotech E25T | 3.29 | 32:1 | 62:1 | 1742.55 | 373.28 | 0.5 | 1.02 | 4.80 | 5.62 | 939 |
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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