DFR Technologies Delta IV Heavy - 18mm
DFR Technologies - Delta IV Heavy - 18mm {Kit} (DIV-HVY-18) [2011-2012]
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 |
---|---|---|---|---|---|---|---|---|---|---|
Estes C5 | 7.74 | 2:1 | 10:1 | 288.27 | 49.78 | 2.1 | 2.03 | 2.20 | 4.03 | 165 |
Estes B4 | 7.67 | 2:1 | 7:1 | 165.76 | 22.84 | 14.4 | 1.05 | 1.10 | 1.95 | 36 |
Weco C6 | 7.74 | 2:1 | 6:1 | 162.88 | 28.69 | 13.9 | 1.71 | 1.30 | 2.81 | 71 |
Estes C6 | 7.81 | 2:1 | 7:1 | 187.09 | 49.53 | 7.1 | 1.96 | 2.10 | 3.86 | 149 |
Estes B6 | 7.64 | 3:1 | 6:1 | 156.52 | 26.98 | 7.7 | 0.89 | 1.30 | 1.99 | 40 |
Aerotech C6W | 7.81 | 3:1 | 6:1 | 145.58 | 65.10 | 3.5 | 1.70 | 2.50 | 4.00 | 209 |
Quest B6 | 7.57 | 3:1 | 7:1 | 194.39 | 31.93 | 5.4 | 0.77 | 1.50 | 2.07 | 48 |
Apogee B7 | 7.32 | 3:1 | 8:1 | 204.35 | 34.18 | 3.0 | 0.81 | 1.50 | 2.11 | 57 |
Aerotech D8 | 7.67 | 4:1 | 8:1 | 207.07 | 120.10 | 2.6 | 2.49 | 4.20 | 6.49 | 631 |
Apogee C10 | 7.62 | 5:1 | 13:1 | 367.56 | 70.01 | 1.9 | 1.03 | 2.90 | 3.73 | 205 |
Aerotech C12T | 7.77 | 6:1 | 11:1 | 280.97 | 69.49 | 2.0 | 0.98 | 2.90 | 3.68 | 193 |
Aerotech D13W | 8.16 | 6:1 | 11:1 | 297.26 | 136.36 | 1.8 | 1.71 | 4.60 | 6.11 | 605 |
Aerotech D10W | 7.91 | 6:1 | 13:1 | 350.21 | 141.37 | 1.9 | 1.41 | 4.80 | 6.01 | 605 |
Apogee D10 | 7.91 | 7:1 | 13:1 | 352.21 | 143.12 | 1.9 | 1.41 | 4.90 | 6.11 | 611 |
Aerotech D21T | 7.88 | 11:1 | 17:1 | 460.73 | 159.63 | 1.3 | 0.99 | 5.20 | 5.99 | 632 |
Aerotech D24T | 8.09 | 11:1 | 21:1 | 348.71 | 129.46 | 1.7 | 0.91 | 4.70 | 5.41 | 472 |
Aerotech E25T | 7.71 | 12:1 | 23:1 | 671.83 | 194.74 | 1.0 | 0.95 | 5.80 | 6.55 | 803 |
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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