Rocket Motor Guide
Estes Mercury Atlas
Estes - Mercury Atlas {Kit} (2111) [1995-1998]
| 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 |
|---|---|---|---|---|---|---|---|---|---|---|
| Weco C6 | 8.54 | 2:1 | 6:1 | 143.37 | 21.13 | 30.7 | 1.72 | 1.00 | 2.52 | 49 |
| Estes C6 | 8.61 | 2:1 | 7:1 | 165.47 | 38.33 | 10.6 | 1.92 | 1.60 | 3.32 | 103 |
| Estes B6 | 8.44 | 2:1 | 6:1 | 138.06 | 21.79 | 10.8 | 0.95 | 0.90 | 1.65 | 28 |
| Aerotech E6RCT | 9.66 | 2:1 | 5:1 | 121.55 | 61.12 | 4.2 | 7.28 | 2.50 | 8.78 | 618 |
| Aerotech E7RCT | 9.51 | 2:1 | 5:1 | 117.25 | 59.79 | 4.4 | 5.80 | 2.00 | 6.80 | 460 |
| Aerotech C6W | 8.61 | 3:1 | 5:1 | 127.79 | 52.31 | 3.9 | 1.63 | 1.80 | 3.23 | 132 |
| Quest B6 | 8.37 | 3:1 | 7:1 | 171.77 | 27.38 | 6.9 | 0.76 | 1.20 | 1.76 | 35 |
| Apogee E6 | 9.43 | 3:1 | 9:1 | 234.37 | 76.16 | 2.7 | 6.17 | 2.50 | 7.67 | 648 |
| Aerotech D7T | 9.29 | 3:1 | 5:1 | 109.67 | 64.41 | 4.4 | 2.94 | 2.20 | 4.94 | 294 |
| Apogee B7 | 8.12 | 3:1 | 7:1 | 180.62 | 29.20 | 3.5 | 0.74 | 1.20 | 1.74 | 41 |
| Aerotech D8 | 8.47 | 3:1 | 7:1 | 181.70 | 82.07 | 2.8 | 2.51 | 2.30 | 4.61 | 323 |
| Aerotech E10 | 9.22 | 4:1 | 9:1 | 218.38 | 136.00 | 2.6 | 4.13 | 2.40 | 6.33 | 669 |
| Estes D11 | 9.38 | 4:1 | 12:1 | 284.44 | 82.87 | 2.3 | 1.95 | 2.60 | 4.35 | 267 |
| Apogee C10 | 8.42 | 5:1 | 12:1 | 328.72 | 57.87 | 2.1 | 1.04 | 2.10 | 2.94 | 130 |
| Aerotech D9W | 9.46 | 5:1 | 9:1 | 207.57 | 97.04 | 4.3 | 1.89 | 2.70 | 4.39 | 284 |
| Estes D12 | 9.30 | 5:1 | 14:1 | 309.41 | 82.76 | 2.2 | 1.75 | 2.60 | 4.15 | 249 |
| Aerotech C12T | 8.57 | 5:1 | 10:1 | 250.71 | 57.40 | 2.2 | 0.99 | 2.10 | 2.89 | 123 |
| Estes C11 | 9.04 | 5:1 | 10:1 | 244.29 | 50.37 | 2.5 | 0.87 | 2.00 | 2.67 | 95 |
| Aerotech E12RCJ | 9.89 | 5:1 | 8:1 | 207.71 | 128.24 | 2.5 | 3.08 | 2.80 | 5.68 | 565 |
| Aerotech D13W | 8.96 | 5:1 | 10:1 | 266.65 | 102.71 | 1.9 | 1.72 | 2.60 | 4.12 | 307 |
| Aerotech E11J | 10.00 | 5:1 | 9:1 | 204.02 | 127.91 | 2.7 | 2.91 | 2.80 | 5.51 | 529 |
| Aerotech D10W | 8.71 | 6:1 | 12:1 | 313.58 | 105.46 | 2.0 | 1.42 | 2.90 | 4.12 | 302 |
| Apogee D10 | 8.71 | 6:1 | 12:1 | 315.42 | 107.59 | 2.0 | 1.43 | 2.90 | 4.13 | 307 |
| Aerotech D15T | 9.35 | 6:1 | 13:1 | 329.69 | 106.14 | 1.6 | 1.50 | 2.70 | 4.00 | 300 |
| Aerotech F12 | 10.15 | 7:1 | 11:1 | 251.80 | 158.00 | 2.0 | 2.94 | 3.00 | 5.74 | 662 |
| Aerotech E15W | 9.57 | 7:1 | 13:1 | 343.99 | 145.53 | 1.6 | 2.70 | 3.10 | 5.60 | 626 |
| Aerotech E18W | 9.81 | 8:1 | 14:1 | 362.84 | 170.46 | 1.5 | 2.20 | 3.20 | 5.20 | 591 |
| Aerotech E20W | 9.53 | 9:1 | 16:1 | 413.69 | 165.92 | 1.4 | 1.85 | 3.30 | 4.95 | 514 |
| Aerotech D21T | 8.68 | 10:1 | 15:1 | 413.39 | 124.36 | 1.4 | 1.00 | 3.10 | 3.90 | 307 |
| Aerotech D24T | 8.89 | 10:1 | 19:1 | 312.93 | 104.80 | 2.0 | 0.92 | 3.00 | 3.72 | 252 |
| CTI 24E22-13A | 9.79 | 10:1 | 14:1 | 360.15 | 145.43 | 2.0 | 1.12 | 3.40 | 4.32 | 373 |
| Aerotech F24 | 10.00 | 10:1 | 19:1 | 466.88 | 188.52 | 1.5 | 2.22 | 3.30 | 5.32 | 660 |
| Aerotech E25T | 8.51 | 11:1 | 21:1 | 602.28 | 146.85 | 1.1 | 0.96 | 3.30 | 4.06 | 362 |
| CTI 26E31-15A | 9.63 | 13:1 | 20:1 | 528.93 | 159.79 | 1.5 | 0.89 | 3.60 | 4.29 | 390 |
| Aerotech E30T | 9.33 | 15:1 | 22:1 | 614.10 | 207.07 | 1.0 | 1.26 | 3.60 | 4.66 | 546 |
| Aerotech E28T | 9.72 | 15:1 | 23:1 | 591.92 | 200.68 | 1.1 | 1.26 | 3.70 | 4.76 | 546 |
| Estes E30T | 9.31 | 15:1 | 23:1 | 625.06 | 182.01 | 1.1 | 1.06 | 3.60 | 4.46 | 462 |
| Aerotech F39 | 9.92 | 17:1 | 27:1 | 707.43 | 229.21 | 0.9 | 1.35 | 3.80 | 4.95 | 640 |
| Aerotech F44W | 9.49 | 20:1 | 30:1 | 800.05 | 253.31 | 1.2 | 1.01 | 3.80 | 4.61 | 542 |
| Aerotech E50 | 9.15 | 24:1 | 25:1 | 647.22 | 254.17 | 1.1 | 0.88 | 3.90 | 4.58 | 545 |
| CTI 25E75-17A | 9.63 | 34:1 | 44:1 | 1181.24 | 158.47 | 0.7 | 0.33 | 3.60 | 3.73 | 305 |
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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