Rocket Motor Guide
Estes Reliant
Estes - Reliant {Kit} (1986) [1988-1997]
| 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 |
|---|---|---|---|---|---|---|---|---|---|---|
| Quest Micro Maxx II | 0.66 | 3:1 | 19:1 | 543.08 | 21.37 | 12.3 | 0.71 | 1.00 | 1.51 | 28 |
| Apogee A2 | 0.86 | 11:1 | 28:1 | 708.96 | 175.40 | 1.1 | 1.40 | 4.40 | 5.60 | 596 |
| Apogee 1/2A2 | 0.78 | 11:1 | 23:1 | 601.84 | 105.85 | 1.2 | 0.70 | 3.60 | 4.10 | 278 |
| Estes A3T | 0.92 | 13:1 | 34:1 | 678.72 | 150.86 | 1.2 | 1.02 | 4.40 | 5.22 | 476 |
| Estes A10T | 0.80 | 14:1 | 73:1 | 1190.58 | 150.01 | 1.0 | 0.90 | 4.10 | 4.80 | 459 |
| Estes 1/4A3T | 0.84 | 14:1 | 29:1 | 606.22 | 28.32 | 1.3 | 0.32 | 1.30 | 1.42 | 29 |
| Apogee 1/4A2 | 0.75 | 14:1 | 31:1 | 781.61 | 35.62 | 1.0 | 0.30 | 1.60 | 1.70 | 42 |
| MPC 1/2A3-M | 0.85 | 17:1 | 29:1 | 519.09 | 78.27 | 1.5 | 0.53 | 2.90 | 3.23 | 171 |
| Estes 1/2A3T | 0.85 | 18:1 | 44:1 | 789.54 | 65.57 | 1.0 | 0.40 | 2.60 | 2.80 | 128 |
| Quest C6 | 1.48 | 18:1 | 90:1 | 1403.73 | 288.98 | 1.6 | 2.55 | 6.30 | 8.65 | 1684 |
| Estes A8 | 1.20 | 18:1 | 56:1 | 703.19 | 125.34 | 1.3 | 0.75 | 4.30 | 4.85 | 396 |
| Estes 1/2A6 | 1.11 | 20:1 | 46:1 | 598.90 | 61.29 | 1.5 | 0.36 | 2.60 | 2.76 | 113 |
| Apogee C4 | 1.22 | 22:1 | 66:1 | 1128.65 | 294.01 | 0.9 | 2.36 | 6.00 | 8.16 | 1677 |
| Estes C5 | 1.37 | 23:1 | 118:1 | 2188.57 | 368.58 | 1.0 | 1.99 | 6.10 | 7.89 | 1724 |
| Estes B4 | 1.29 | 24:1 | 74:1 | 869.28 | 219.78 | 1.0 | 1.10 | 5.50 | 6.40 | 823 |
| Weco C6 | 1.36 | 27:1 | 72:1 | 1384.72 | 293.40 | 1.2 | 1.79 | 5.80 | 7.39 | 1277 |
| Estes C6 | 1.44 | 27:1 | 82:1 | 1182.47 | 371.72 | 1.2 | 1.91 | 6.40 | 8.11 | 1634 |
| Estes B6 | 1.26 | 29:1 | 70:1 | 953.56 | 235.10 | 1.2 | 0.91 | 5.60 | 6.31 | 835 |
| Quest A6 | 1.16 | 29:1 | 69:1 | 1125.02 | 126.00 | 1.3 | 0.41 | 4.20 | 4.41 | 354 |
| Quest A8 Q-Jet | 1.08 | 30:1 | 65:1 | 1155.08 | 129.59 | 1.4 | 0.42 | 4.10 | 4.32 | 344 |
| FSI A6 | 1.19 | 32:1 | 67:1 | 1180.00 | 100.92 | 1.2 | 0.50 | 3.50 | 3.80 | 252 |
| Aerotech C6W | 1.43 | 35:1 | 68:1 | 1034.30 | 405.02 | 1.2 | 1.69 | 6.60 | 8.09 | 1673 |
| Quest B6 | 1.19 | 36:1 | 83:1 | 1494.03 | 298.20 | 1.1 | 0.79 | 5.80 | 6.39 | 953 |
| Apogee B7 | 0.94 | 39:1 | 86:1 | 1689.18 | 326.23 | 0.8 | 0.84 | 5.50 | 6.14 | 958 |
| Aerotech D8 | 1.29 | 41:1 | 89:1 | 1741.57 | 623.07 | 0.7 | 2.44 | 6.20 | 8.44 | 2523 |
| Apogee C10 | 1.24 | 58:1 | 149:1 | 2518.92 | 450.02 | 0.6 | 1.04 | 6.50 | 7.34 | 1492 |
| Aerotech C12T | 1.39 | 62:1 | 119:1 | 1792.88 | 431.09 | 0.9 | 0.96 | 6.90 | 7.66 | 1541 |
| Aerotech D13W | 1.78 | 65:1 | 129:1 | 1756.98 | 610.98 | 0.5 | 1.72 | 7.50 | 9.02 | 2477 |
| Aerotech D10W | 1.53 | 72:1 | 145:1 | 2383.20 | 674.80 | 0.5 | 1.42 | 7.20 | 8.42 | 2334 |
| Apogee D10 | 1.53 | 78:1 | 146:1 | 2413.93 | 683.52 | 0.5 | 1.42 | 7.20 | 8.42 | 2355 |
| Aerotech D21T | 1.50 | 121:1 | 186:1 | 3002.28 | 789.40 | 0.5 | 1.03 | 7.30 | 8.13 | 2252 |
| Aerotech D24T | 1.71 | 126:1 | 239:1 | 1803.33 | 643.88 | 0.6 | 0.93 | 7.80 | 8.53 | 2159 |
| Aerotech E25T | 1.33 | 135:1 | 258:1 | 4918.70 | 958.70 | 0.4 | 1.01 | 6.70 | 7.51 | 2271 |
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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