Estes USSF Fireflash
Estes - USSF Fireflash {Kit} (1909)
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 | 1.94 | 4:1 | 10:1 | 272.42 | 72.95 | 4.1 | 1.37 | 3.00 | 4.17 | 216 |
Apogee 1/2A2 | 1.86 | 4:1 | 8:1 | 222.63 | 38.14 | 4.4 | 0.69 | 1.70 | 2.19 | 61 |
Estes A3T | 2.00 | 5:1 | 12:1 | 325.74 | 62.30 | 2.0 | 1.09 | 2.60 | 3.49 | 163 |
Estes A10T | 1.88 | 5:1 | 27:1 | 640.05 | 40.73 | 1.3 | 0.94 | 1.80 | 2.54 | 81 |
Apogee 1/4A2 | 1.83 | 5:1 | 11:1 | 314.99 | 20.13 | 3.0 | 0.31 | 1.00 | 1.11 | 14 |
MPC 1/2A3-M | 1.93 | 6:1 | 11:1 | 279.66 | 29.74 | 2.2 | 0.51 | 1.40 | 1.71 | 37 |
Estes 1/2A3T | 1.93 | 6:1 | 16:1 | 440.74 | 28.52 | 1.4 | 0.44 | 1.30 | 1.54 | 33 |
Quest C6 | 2.56 | 7:1 | 33:1 | 683.39 | 170.92 | 2.0 | 2.61 | 5.20 | 7.61 | 961 |
Estes A8 | 2.28 | 7:1 | 21:1 | 437.73 | 49.77 | 1.7 | 0.80 | 2.20 | 2.80 | 104 |
Estes 1/2A6 | 2.19 | 7:1 | 17:1 | 380.56 | 20.37 | 1.8 | 0.41 | 1.00 | 1.21 | 16 |
Apogee C4 | 2.30 | 8:1 | 24:1 | 542.73 | 182.89 | 1.5 | 2.40 | 5.30 | 7.50 | 1040 |
Estes C5 | 2.44 | 8:1 | 43:1 | 1046.76 | 222.23 | 1.3 | 2.02 | 5.70 | 7.52 | 1092 |
Estes B4 | 2.37 | 9:1 | 27:1 | 619.86 | 103.21 | 1.2 | 1.13 | 3.80 | 4.73 | 339 |
Weco C6 | 2.44 | 10:1 | 26:1 | 452.79 | 155.18 | 1.5 | 1.74 | 4.90 | 6.44 | 676 |
Estes C6 | 2.52 | 10:1 | 30:1 | 543.88 | 206.71 | 1.4 | 1.95 | 5.60 | 7.35 | 948 |
Estes B6 | 2.34 | 11:1 | 26:1 | 507.97 | 112.28 | 1.4 | 0.95 | 4.00 | 4.75 | 365 |
Quest A6 | 2.24 | 11:1 | 25:1 | 448.08 | 49.06 | 1.6 | 0.46 | 2.20 | 2.46 | 85 |
Quest A8 Q-Jet | 2.16 | 11:1 | 24:1 | 509.00 | 54.92 | 1.8 | 0.38 | 2.40 | 2.58 | 95 |
FSI A6 | 2.27 | 12:1 | 24:1 | 466.52 | 49.14 | 1.5 | 0.54 | 2.00 | 2.34 | 79 |
Aerotech C6W | 2.51 | 13:1 | 25:1 | 544.11 | 236.44 | 1.5 | 1.63 | 5.90 | 7.33 | 1068 |
Quest B6 | 2.27 | 13:1 | 30:1 | 515.36 | 130.07 | 1.5 | 0.83 | 4.40 | 5.03 | 432 |
Apogee B7 | 2.02 | 14:1 | 31:1 | 671.66 | 150.19 | 1.2 | 0.78 | 4.70 | 5.28 | 512 |
Aerotech D8 | 2.37 | 15:1 | 32:1 | 816.30 | 360.64 | 1.0 | 2.47 | 6.20 | 8.47 | 1867 |
Apogee C10 | 2.32 | 21:1 | 54:1 | 1353.15 | 250.46 | 0.7 | 1.05 | 5.90 | 6.75 | 989 |
Aerotech C12T | 2.47 | 23:1 | 44:1 | 905.15 | 243.25 | 1.1 | 0.99 | 6.10 | 6.89 | 968 |
Aerotech D13W | 2.86 | 24:1 | 47:1 | 990.22 | 389.98 | 0.7 | 1.74 | 6.90 | 8.44 | 1755 |
Aerotech D10W | 2.61 | 26:1 | 53:1 | 1243.17 | 417.40 | 0.7 | 1.43 | 6.90 | 8.13 | 1714 |
Apogee D10 | 2.61 | 28:1 | 53:1 | 1249.98 | 422.83 | 0.7 | 1.44 | 6.90 | 8.14 | 1724 |
Aerotech D21T | 2.58 | 44:1 | 68:1 | 1624.53 | 485.24 | 0.6 | 1.04 | 7.10 | 7.94 | 1696 |
Aerotech D24T | 2.79 | 46:1 | 87:1 | 1170.02 | 400.92 | 0.7 | 0.94 | 7.20 | 7.94 | 1530 |
Aerotech E25T | 2.41 | 49:1 | 94:1 | 2461.23 | 583.09 | 0.5 | 1.02 | 7.00 | 7.82 | 1843 |
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.
Sponsored Ads