Estes Crossfire ISX
Estes - Crossfire ISX {Kit} (7220) [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 A2 | 1.54 | 5:1 | 13:1 | 357.07 | 95.02 | 2.6 | 1.39 | 3.40 | 4.59 | 304 |
Apogee 1/2A2 | 1.46 | 5:1 | 11:1 | 294.84 | 51.59 | 2.9 | 0.70 | 2.20 | 2.70 | 100 |
Estes A3T | 1.60 | 6:1 | 16:1 | 421.50 | 82.68 | 1.5 | 1.06 | 3.10 | 3.96 | 231 |
Estes A10T | 1.49 | 7:1 | 35:1 | 708.03 | 52.05 | 1.2 | 0.93 | 2.20 | 2.93 | 117 |
Estes 1/4A3T | 1.52 | 7:1 | 14:1 | 352.35 | 20.16 | 1.8 | 0.27 | 1.00 | 1.07 | 13 |
Apogee 1/4A2 | 1.43 | 7:1 | 15:1 | 413.54 | 20.27 | 1.8 | 0.25 | 1.00 | 1.05 | 13 |
MPC 1/2A3-M | 1.53 | 8:1 | 14:1 | 359.81 | 39.19 | 1.9 | 0.48 | 1.70 | 1.98 | 56 |
Estes 1/2A3T | 1.53 | 8:1 | 21:1 | 568.95 | 35.71 | 1.3 | 0.43 | 1.60 | 1.83 | 48 |
Quest C6 | 2.16 | 9:1 | 43:1 | 784.14 | 195.09 | 1.8 | 2.59 | 5.20 | 7.59 | 1086 |
Estes A8 | 1.88 | 9:1 | 27:1 | 476.39 | 62.65 | 1.6 | 0.78 | 2.60 | 3.18 | 145 |
Estes 1/2A6 | 1.79 | 9:1 | 22:1 | 429.11 | 26.18 | 1.7 | 0.39 | 1.20 | 1.39 | 25 |
Apogee C4 | 1.90 | 10:1 | 31:1 | 661.77 | 201.96 | 1.3 | 2.39 | 5.20 | 7.39 | 1120 |
Estes C5 | 2.05 | 11:1 | 56:1 | 1372.45 | 249.87 | 1.2 | 2.01 | 5.50 | 7.31 | 1163 |
Estes B4 | 1.97 | 12:1 | 35:1 | 713.78 | 125.04 | 1.1 | 1.12 | 4.10 | 5.02 | 424 |
Weco C6 | 2.04 | 13:1 | 34:1 | 645.83 | 185.70 | 1.4 | 1.72 | 5.00 | 6.52 | 783 |
Estes C6 | 2.12 | 13:1 | 39:1 | 607.48 | 237.91 | 1.3 | 1.94 | 5.50 | 7.24 | 1041 |
Estes B6 | 1.94 | 14:1 | 34:1 | 564.26 | 137.23 | 1.4 | 0.94 | 4.40 | 5.14 | 453 |
Quest A6 | 1.84 | 14:1 | 33:1 | 488.76 | 62.75 | 1.5 | 0.44 | 2.60 | 2.84 | 125 |
Quest A8 Q-Jet | 1.76 | 14:1 | 31:1 | 784.07 | 77.32 | 1.6 | 0.46 | 3.00 | 3.26 | 172 |
FSI A6 | 1.87 | 15:1 | 32:1 | 641.17 | 63.88 | 1.4 | 0.52 | 2.50 | 2.82 | 121 |
Aerotech C6W | 2.11 | 17:1 | 33:1 | 660.26 | 271.86 | 1.4 | 1.62 | 5.70 | 7.12 | 1122 |
Quest B6 | 1.87 | 17:1 | 40:1 | 583.28 | 163.34 | 1.4 | 0.82 | 4.70 | 5.32 | 527 |
Apogee B7 | 1.62 | 19:1 | 41:1 | 886.16 | 186.34 | 1.1 | 0.76 | 4.80 | 5.36 | 591 |
Aerotech D8 | 1.97 | 20:1 | 42:1 | 1014.71 | 411.18 | 0.8 | 2.46 | 5.70 | 7.96 | 1841 |
Apogee C10 | 1.92 | 28:1 | 71:1 | 1668.55 | 291.58 | 0.6 | 1.04 | 5.70 | 6.54 | 1027 |
Aerotech C12T | 2.07 | 30:1 | 57:1 | 1115.94 | 283.44 | 1.0 | 0.98 | 5.90 | 6.68 | 1025 |
Aerotech D13W | 2.47 | 31:1 | 62:1 | 1182.44 | 432.23 | 0.7 | 1.73 | 6.50 | 8.03 | 1742 |
Aerotech D10W | 2.22 | 35:1 | 69:1 | 1514.90 | 464.05 | 0.6 | 1.42 | 6.40 | 7.62 | 1683 |
Apogee D10 | 2.22 | 37:1 | 69:1 | 1523.27 | 470.23 | 0.6 | 1.43 | 6.40 | 7.63 | 1695 |
Aerotech D21T | 2.18 | 58:1 | 89:1 | 1982.32 | 542.02 | 0.5 | 1.03 | 6.60 | 7.43 | 1643 |
Aerotech D24T | 2.40 | 60:1 | 114:1 | 1316.90 | 450.32 | 0.7 | 0.94 | 6.80 | 7.54 | 1521 |
Aerotech E25T | 2.01 | 64:1 | 123:1 | 2975.05 | 648.65 | 0.4 | 1.02 | 6.30 | 7.12 | 1741 |
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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