Rocket Motor Guide
Estes Starship Nova
Estes - Starship Nova {Kit} (7262) [2017-]
| 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 | 2.34 | 3:1 | 8:1 | 218.00 | 56.50 | 5.9 | 1.37 | 2.40 | 3.57 | 150 |
| Apogee 1/2A2 | 2.25 | 3:1 | 7:1 | 176.53 | 29.12 | 6.0 | 0.69 | 1.30 | 1.79 | 39 |
| Estes A3T | 2.40 | 4:1 | 10:1 | 263.32 | 52.42 | 3.1 | 1.05 | 2.30 | 3.15 | 122 |
| Estes A10T | 2.29 | 4:1 | 22:1 | 579.48 | 34.28 | 1.3 | 0.85 | 1.60 | 2.25 | 61 |
| MPC 1/2A3-M | 2.33 | 5:1 | 9:1 | 224.64 | 26.69 | 2.8 | 0.45 | 1.20 | 1.45 | 28 |
| Estes 1/2A3T | 2.33 | 5:1 | 13:1 | 357.55 | 25.31 | 1.8 | 0.37 | 1.20 | 1.37 | 24 |
| Quest C6 | 2.96 | 5:1 | 27:1 | 608.44 | 150.17 | 2.1 | 2.62 | 5.00 | 7.42 | 842 |
| Estes A8 | 2.67 | 5:1 | 17:1 | 391.22 | 43.03 | 1.8 | 0.81 | 1.90 | 2.51 | 80 |
| Estes 1/2A6 | 2.59 | 6:1 | 13:1 | 331.78 | 20.28 | 2.0 | 0.43 | 0.90 | 1.13 | 14 |
| Apogee C4 | 2.70 | 7:1 | 19:1 | 459.39 | 162.65 | 1.7 | 2.42 | 5.20 | 7.42 | 930 |
| Estes C5 | 2.84 | 7:1 | 35:1 | 828.68 | 195.91 | 1.3 | 2.03 | 5.70 | 7.53 | 996 |
| Estes B4 | 2.77 | 7:1 | 22:1 | 544.87 | 88.08 | 1.3 | 1.04 | 3.50 | 4.34 | 276 |
| Weco C6 | 2.84 | 8:1 | 21:1 | 413.11 | 129.49 | 1.7 | 1.75 | 4.60 | 6.15 | 559 |
| Estes C6 | 2.91 | 8:1 | 24:1 | 492.52 | 180.74 | 1.5 | 1.96 | 5.40 | 7.16 | 846 |
| Estes B6 | 2.74 | 9:1 | 21:1 | 475.64 | 95.31 | 1.5 | 0.86 | 3.80 | 4.46 | 292 |
| Quest A6 | 2.64 | 9:1 | 20:1 | 417.05 | 40.08 | 1.7 | 0.47 | 1.80 | 2.07 | 61 |
| Quest A8 Q-Jet | 2.56 | 9:1 | 19:1 | 363.84 | 39.53 | 1.9 | 0.40 | 1.80 | 2.00 | 54 |
| FSI A6 | 2.67 | 9:1 | 20:1 | 421.04 | 31.46 | 1.6 | 0.55 | 1.30 | 1.65 | 35 |
| Aerotech C6W | 2.91 | 10:1 | 20:1 | 461.11 | 207.62 | 1.6 | 1.64 | 5.80 | 7.24 | 984 |
| Quest B6 | 2.67 | 11:1 | 25:1 | 478.10 | 108.62 | 1.5 | 0.84 | 4.00 | 4.64 | 344 |
| Apogee B7 | 2.42 | 12:1 | 25:1 | 659.03 | 125.93 | 1.3 | 0.78 | 4.40 | 4.98 | 432 |
| Aerotech D8 | 2.77 | 12:1 | 26:1 | 680.49 | 322.26 | 1.0 | 2.47 | 6.60 | 8.87 | 1842 |
| Apogee C10 | 2.72 | 17:1 | 44:1 | 1136.42 | 217.45 | 0.7 | 1.05 | 5.90 | 6.75 | 914 |
| Aerotech C12T | 2.87 | 18:1 | 35:1 | 758.91 | 211.19 | 1.2 | 1.00 | 6.00 | 6.80 | 886 |
| Aerotech D13W | 3.26 | 19:1 | 38:1 | 850.53 | 353.62 | 0.8 | 1.74 | 7.10 | 8.64 | 1721 |
| Aerotech D10W | 3.01 | 21:1 | 43:1 | 1052.61 | 377.70 | 0.8 | 1.44 | 7.20 | 8.44 | 1695 |
| Apogee D10 | 3.01 | 23:1 | 43:1 | 1058.36 | 382.55 | 0.8 | 1.44 | 7.20 | 8.44 | 1707 |
| Aerotech D21T | 2.98 | 36:1 | 55:1 | 1374.65 | 432.88 | 0.6 | 0.94 | 7.50 | 8.24 | 1693 |
| Aerotech D24T | 3.19 | 37:1 | 71:1 | 1002.29 | 357.92 | 0.8 | 0.95 | 7.40 | 8.15 | 1496 |
| Aerotech E25T | 2.81 | 40:1 | 76:1 | 2094.60 | 525.23 | 0.5 | 1.02 | 7.40 | 8.22 | 1882 |
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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