Estes Plasma Probe
Estes - Plasma Probe {Kit} (003211)
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 |
---|---|---|---|---|---|---|---|---|---|---|
Aerotech D8 | 12.47 | 2:1 | 5:1 | 113.08 | 66.24 | 4.3 | 2.51 | 2.80 | 5.11 | 295 |
Apogee C10 | 12.42 | 3:1 | 8:1 | 210.89 | 38.13 | 3.5 | 1.03 | 1.70 | 2.53 | 79 |
Aerotech C12T | 12.57 | 3:1 | 6:1 | 159.98 | 37.98 | 3.5 | 0.98 | 1.70 | 2.48 | 75 |
Aerotech D13W | 12.96 | 3:1 | 7:1 | 171.93 | 81.14 | 2.8 | 1.78 | 3.20 | 4.78 | 314 |
Aerotech D10W | 12.71 | 4:1 | 8:1 | 201.79 | 82.88 | 3.0 | 1.39 | 3.60 | 4.79 | 310 |
Apogee D10 | 12.71 | 4:1 | 8:1 | 203.01 | 83.48 | 3.0 | 1.49 | 3.50 | 4.79 | 312 |
Aerotech D21T | 12.68 | 6:1 | 10:1 | 269.02 | 95.67 | 2.0 | 1.04 | 4.00 | 4.84 | 346 |
Aerotech D24T | 12.89 | 7:1 | 13:1 | 203.09 | 79.69 | 2.9 | 0.99 | 3.50 | 4.29 | 254 |
Aerotech E25T | 12.51 | 7:1 | 14:1 | 393.10 | 118.62 | 1.6 | 0.99 | 4.90 | 5.69 | 499 |
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