Estes V-2
Estes - V-2 {Kit} (3228) [2012-]
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 C4 | 6.90 | 2:1 | 6:1 | 152.12 | 38.86 | 3.7 | 2.38 | 1.70 | 3.88 | 153 |
Estes C5 | 7.04 | 2:1 | 12:1 | 320.48 | 52.17 | 2.0 | 2.01 | 2.10 | 3.91 | 169 |
Estes B4 | 6.97 | 2:1 | 7:1 | 186.10 | 26.40 | 10.0 | 1.05 | 1.20 | 2.05 | 44 |
Weco C6 | 7.04 | 3:1 | 7:1 | 182.91 | 33.35 | 7.6 | 1.75 | 1.50 | 3.05 | 87 |
Estes C6 | 7.11 | 3:1 | 8:1 | 209.46 | 53.57 | 5.2 | 1.87 | 2.20 | 3.87 | 158 |
Estes B6 | 6.94 | 3:1 | 7:1 | 175.88 | 30.10 | 5.8 | 0.90 | 1.40 | 2.10 | 47 |
Aerotech E6RCT | 8.16 | 3:1 | 7:1 | 152.77 | 85.85 | 3.5 | 7.23 | 3.00 | 9.23 | 903 |
Aerotech E7RCT | 8.01 | 3:1 | 7:1 | 147.58 | 83.23 | 3.7 | 5.75 | 3.00 | 7.75 | 683 |
Aerotech C6W | 7.11 | 3:1 | 7:1 | 162.40 | 68.63 | 3.2 | 1.68 | 2.30 | 3.78 | 199 |
Quest B6 | 6.87 | 4:1 | 8:1 | 217.79 | 35.11 | 4.3 | 0.82 | 1.50 | 2.12 | 56 |
Apogee E6 | 7.93 | 4:1 | 11:1 | 290.16 | 105.81 | 2.2 | 6.14 | 3.50 | 8.64 | 924 |
Aerotech D7T | 7.79 | 4:1 | 6:1 | 138.37 | 87.47 | 3.5 | 2.88 | 3.00 | 5.68 | 430 |
Apogee B7 | 6.62 | 4:1 | 8:1 | 229.52 | 38.98 | 2.7 | 0.79 | 1.60 | 2.19 | 67 |
Aerotech D8 | 6.97 | 4:1 | 9:1 | 230.38 | 107.55 | 2.4 | 2.47 | 3.00 | 5.27 | 469 |
Aerotech E10 | 7.72 | 5:1 | 11:1 | 270.41 | 176.10 | 2.2 | 4.10 | 3.20 | 7.10 | 939 |
QUEST D8 | 22.31 | 5:1 | 17:1 | 122.84 | 21.18 | 22.3 | 2.25 | 1.00 | 3.05 | 62 |
Estes D11 | 7.88 | 5:1 | 15:1 | 324.53 | 109.51 | 2.1 | 1.93 | 3.40 | 5.13 | 398 |
Apogee C10 | 6.92 | 6:1 | 15:1 | 408.90 | 73.64 | 1.7 | 1.01 | 2.60 | 3.41 | 189 |
Estes D12 | 7.80 | 6:1 | 17:1 | 339.79 | 107.98 | 2.0 | 1.73 | 3.30 | 4.83 | 368 |
Aerotech C12T | 7.07 | 6:1 | 12:1 | 312.09 | 73.60 | 1.9 | 0.96 | 2.70 | 3.46 | 182 |
Estes C11 | 7.55 | 6:1 | 12:1 | 281.22 | 65.80 | 2.3 | 0.85 | 2.50 | 3.15 | 144 |
Aerotech E12RCJ | 8.40 | 6:1 | 10:1 | 256.84 | 166.24 | 2.1 | 3.05 | 3.70 | 6.55 | 796 |
Aerotech D13W | 7.46 | 6:1 | 13:1 | 329.58 | 131.34 | 1.6 | 1.80 | 3.30 | 4.90 | 442 |
Aerotech E11J | 8.50 | 7:1 | 11:1 | 251.52 | 165.29 | 2.3 | 2.88 | 3.60 | 6.28 | 747 |
Aerotech D10W | 7.21 | 7:1 | 14:1 | 389.05 | 135.71 | 1.7 | 1.40 | 3.60 | 4.80 | 436 |
Apogee D10 | 7.21 | 8:1 | 14:1 | 391.29 | 136.17 | 1.7 | 1.40 | 3.60 | 4.80 | 436 |
Aerotech D15T | 7.85 | 8:1 | 16:1 | 396.25 | 133.57 | 1.4 | 1.48 | 3.50 | 4.78 | 430 |
Aerotech F12 | 8.65 | 8:1 | 13:1 | 307.08 | 206.34 | 1.7 | 3.02 | 3.80 | 6.62 | 930 |
Aerotech E15W | 8.07 | 9:1 | 16:1 | 420.72 | 189.73 | 1.4 | 2.69 | 4.00 | 6.49 | 877 |
Aerotech E18W | 8.31 | 10:1 | 18:1 | 440.98 | 217.58 | 1.3 | 2.29 | 4.00 | 6.09 | 831 |
Aerotech E20W | 8.03 | 11:1 | 20:1 | 500.90 | 211.40 | 1.2 | 1.83 | 4.10 | 5.73 | 728 |
Aerotech D21T | 7.18 | 12:1 | 18:1 | 511.00 | 158.06 | 1.2 | 0.98 | 3.90 | 4.68 | 441 |
Aerotech D24T | 7.39 | 12:1 | 24:1 | 386.28 | 132.01 | 1.6 | 0.90 | 3.70 | 4.40 | 359 |
CTI 24E22-13A | 8.29 | 13:1 | 18:1 | 437.82 | 181.92 | 1.7 | 1.09 | 4.20 | 5.09 | 532 |
Aerotech F24 | 8.50 | 13:1 | 23:1 | 561.37 | 240.55 | 1.4 | 2.21 | 4.20 | 6.21 | 929 |
Aerotech E25T | 7.01 | 13:1 | 25:1 | 745.88 | 188.24 | 0.9 | 0.95 | 4.10 | 4.85 | 517 |
CTI 26E31-15A | 8.13 | 17:1 | 25:1 | 640.52 | 203.67 | 1.3 | 0.87 | 4.40 | 5.07 | 559 |
Aerotech E30T | 7.83 | 19:1 | 28:1 | 750.18 | 263.78 | 0.9 | 1.25 | 4.50 | 5.55 | 773 |
Aerotech E28T | 8.22 | 19:1 | 29:1 | 707.59 | 253.67 | 0.9 | 1.25 | 4.50 | 5.55 | 772 |
Estes E30T | 7.81 | 19:1 | 28:1 | 762.25 | 231.32 | 0.9 | 1.05 | 4.40 | 5.25 | 655 |
Aerotech F39 | 8.42 | 21:1 | 34:1 | 845.83 | 292.45 | 0.8 | 1.34 | 4.70 | 5.84 | 903 |
Aerotech F44W | 7.99 | 24:1 | 37:1 | 969.38 | 320.16 | 1.1 | 1.00 | 4.60 | 5.40 | 774 |
Aerotech E50 | 7.65 | 30:1 | 31:1 | 797.50 | 321.56 | 0.9 | 0.87 | 4.70 | 5.37 | 768 |
CTI 25E75-17A | 8.13 | 42:1 | 54:1 | 1421.58 | 188.83 | 0.7 | 0.33 | 4.30 | 4.43 | 431 |
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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