Rocket Motor Guide
Estes Satellite Interceptor
Estes - Satellite Interceptor {Kit} (1296, 3027) [1978-1982]
| 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 | 2.54 | 3:1 | 8:1 | 197.32 | 48.34 | 6.9 | 1.33 | 2.10 | 3.23 | 117 |
| Apogee 1/2A2 | 2.46 | 3:1 | 6:1 | 159.07 | 24.25 | 7.0 | 0.65 | 1.10 | 1.55 | 28 |
| Estes A3T | 2.60 | 3:1 | 9:1 | 239.43 | 44.70 | 4.0 | 1.09 | 2.00 | 2.89 | 99 |
| Estes A10T | 2.48 | 4:1 | 20:1 | 551.76 | 32.12 | 1.4 | 0.86 | 1.50 | 2.16 | 56 |
| MPC 1/2A3-M | 2.53 | 5:1 | 8:1 | 203.64 | 23.89 | 3.4 | 0.48 | 1.10 | 1.38 | 24 |
| Estes 1/2A3T | 2.53 | 5:1 | 12:1 | 325.78 | 24.57 | 2.2 | 0.39 | 1.20 | 1.39 | 23 |
| Quest C6 | 3.16 | 5:1 | 24:1 | 576.82 | 141.09 | 2.1 | 2.63 | 4.90 | 7.33 | 787 |
| Estes A8 | 2.88 | 5:1 | 15:1 | 366.67 | 40.55 | 1.8 | 0.82 | 1.80 | 2.42 | 72 |
| Estes 1/2A6 | 2.79 | 5:1 | 12:1 | 304.76 | 20.28 | 2.1 | 0.34 | 1.00 | 1.14 | 14 |
| Apogee C4 | 2.90 | 6:1 | 18:1 | 427.04 | 153.02 | 1.8 | 2.43 | 5.10 | 7.33 | 871 |
| Estes C5 | 3.04 | 6:1 | 32:1 | 735.63 | 183.55 | 1.4 | 2.04 | 5.60 | 7.44 | 943 |
| Estes B4 | 2.97 | 7:1 | 20:1 | 502.87 | 81.91 | 1.4 | 1.04 | 3.40 | 4.24 | 250 |
| Weco C6 | 3.04 | 7:1 | 19:1 | 397.24 | 119.85 | 1.7 | 1.76 | 4.40 | 5.96 | 513 |
| Estes C6 | 3.11 | 7:1 | 22:1 | 470.87 | 169.36 | 1.5 | 1.86 | 5.50 | 7.16 | 798 |
| Estes B6 | 2.94 | 8:1 | 19:1 | 462.88 | 88.83 | 1.6 | 0.87 | 3.60 | 4.27 | 266 |
| Quest A6 | 2.84 | 8:1 | 18:1 | 402.13 | 36.66 | 1.8 | 0.48 | 1.70 | 1.98 | 52 |
| Quest A8 Q-Jet | 2.76 | 8:1 | 17:1 | 342.04 | 34.55 | 2.0 | 0.41 | 1.60 | 1.81 | 42 |
| FSI A6 | 2.87 | 9:1 | 18:1 | 395.21 | 26.77 | 1.7 | 0.56 | 1.10 | 1.46 | 27 |
| Aerotech C6W | 3.11 | 9:1 | 18:1 | 430.46 | 195.07 | 1.7 | 1.65 | 5.80 | 7.25 | 940 |
| Quest B6 | 2.87 | 10:1 | 23:1 | 463.79 | 101.44 | 1.6 | 0.85 | 3.90 | 4.55 | 312 |
| Apogee B7 | 2.62 | 11:1 | 23:1 | 644.35 | 116.44 | 1.3 | 0.79 | 4.30 | 4.89 | 395 |
| Aerotech D8 | 2.97 | 11:1 | 24:1 | 627.34 | 308.82 | 1.1 | 2.48 | 6.70 | 8.98 | 1824 |
| Apogee C10 | 2.92 | 16:1 | 40:1 | 1050.93 | 203.54 | 0.8 | 1.05 | 5.90 | 6.75 | 873 |
| Aerotech C12T | 3.07 | 17:1 | 32:1 | 699.54 | 197.47 | 1.2 | 1.00 | 5.90 | 6.70 | 842 |
| Aerotech D13W | 3.46 | 18:1 | 35:1 | 793.62 | 337.04 | 0.8 | 1.74 | 7.20 | 8.74 | 1699 |
| Aerotech D10W | 3.21 | 20:1 | 39:1 | 976.58 | 359.92 | 0.8 | 1.44 | 7.30 | 8.54 | 1681 |
| Apogee D10 | 3.21 | 21:1 | 39:1 | 981.91 | 364.37 | 0.8 | 1.44 | 7.30 | 8.54 | 1693 |
| Aerotech D21T | 3.18 | 33:1 | 50:1 | 1275.18 | 409.61 | 0.7 | 0.94 | 7.60 | 8.34 | 1685 |
| Aerotech D24T | 3.39 | 34:1 | 65:1 | 934.26 | 339.07 | 0.8 | 0.95 | 7.50 | 8.25 | 1474 |
| Aerotech E25T | 3.01 | 36:1 | 70:1 | 1931.77 | 498.48 | 0.5 | 1.02 | 7.60 | 8.42 | 1894 |
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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