Estes Black Star Voyager
Estes - Black Star Voyager {Kit} (7222) [2012-]
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 |
---|---|---|---|---|---|---|---|---|---|---|
Estes C5 | 7.74 | 2:1 | 10:1 | 288.27 | 49.77 | 2.1 | 2.03 | 2.20 | 4.03 | 165 |
Estes B4 | 7.67 | 2:1 | 7:1 | 165.76 | 22.83 | 14.4 | 1.05 | 1.10 | 1.95 | 36 |
Weco C6 | 7.74 | 2:1 | 6:1 | 162.88 | 28.69 | 13.9 | 1.71 | 1.30 | 2.81 | 71 |
Estes C6 | 7.81 | 2:1 | 7:1 | 187.09 | 49.52 | 7.1 | 1.96 | 2.10 | 3.86 | 149 |
Estes B6 | 7.64 | 3:1 | 6:1 | 156.52 | 26.98 | 7.7 | 0.89 | 1.30 | 1.99 | 40 |
Aerotech E6RCT | 8.86 | 3:1 | 6:1 | 137.55 | 119.05 | 3.7 | 7.25 | 4.50 | 10.75 | 1228 |
Aerotech E7RCT | 8.71 | 3:1 | 6:1 | 132.78 | 106.36 | 3.9 | 5.77 | 4.00 | 8.77 | 891 |
Aerotech C6W | 7.81 | 3:1 | 6:1 | 145.58 | 65.09 | 3.5 | 1.70 | 2.50 | 4.00 | 208 |
Quest B6 | 7.57 | 3:1 | 7:1 | 194.39 | 31.93 | 5.4 | 0.77 | 1.50 | 2.07 | 48 |
Apogee E6 | 8.63 | 3:1 | 10:1 | 262.14 | 146.66 | 2.3 | 6.15 | 5.00 | 10.15 | 1317 |
Aerotech D7T | 8.49 | 3:1 | 6:1 | 124.28 | 98.22 | 3.9 | 2.90 | 3.80 | 6.50 | 526 |
Apogee B7 | 7.32 | 3:1 | 8:1 | 204.35 | 34.18 | 3.0 | 0.81 | 1.50 | 2.11 | 57 |
Aerotech D8 | 7.67 | 4:1 | 8:1 | 207.07 | 120.01 | 2.6 | 2.49 | 4.20 | 6.49 | 630 |
Aerotech E10 | 8.42 | 4:1 | 10:1 | 250.05 | 205.98 | 2.4 | 4.12 | 5.40 | 9.32 | 1488 |
Estes D11 | 8.58 | 5:1 | 13:1 | 304.94 | 112.92 | 2.2 | 1.94 | 4.30 | 6.04 | 488 |
Apogee C10 | 7.62 | 5:1 | 13:1 | 367.56 | 70.00 | 1.9 | 1.03 | 2.90 | 3.73 | 204 |
Aerotech D9W | 8.66 | 5:1 | 10:1 | 236.16 | 124.40 | 4.0 | 1.96 | 4.40 | 6.16 | 531 |
Estes D12 | 8.50 | 5:1 | 15:1 | 327.11 | 110.53 | 2.1 | 1.74 | 4.20 | 5.74 | 452 |
Aerotech C12T | 7.77 | 6:1 | 11:1 | 280.97 | 69.48 | 2.0 | 0.98 | 2.90 | 3.68 | 193 |
Estes C11 | 8.24 | 6:1 | 11:1 | 265.30 | 60.05 | 2.4 | 0.86 | 2.60 | 3.26 | 141 |
Aerotech E12RCJ | 9.09 | 6:1 | 9:1 | 232.03 | 198.80 | 2.3 | 3.07 | 5.70 | 8.57 | 1232 |
Aerotech D13W | 8.16 | 6:1 | 11:1 | 297.26 | 136.29 | 1.8 | 1.71 | 4.60 | 6.11 | 604 |
Aerotech E11J | 9.20 | 6:1 | 10:1 | 232.21 | 193.96 | 2.4 | 2.90 | 5.60 | 8.30 | 1141 |
Aerotech D10W | 7.91 | 6:1 | 13:1 | 350.21 | 141.31 | 1.9 | 1.41 | 4.80 | 6.01 | 604 |
Apogee D10 | 7.91 | 7:1 | 13:1 | 352.21 | 143.06 | 1.9 | 1.41 | 4.90 | 6.11 | 610 |
Aerotech D15T | 8.55 | 7:1 | 15:1 | 363.66 | 135.39 | 1.5 | 1.49 | 4.60 | 5.89 | 582 |
Aerotech F12 | 9.35 | 8:1 | 12:1 | 284.63 | 254.94 | 1.9 | 3.03 | 6.20 | 9.03 | 1517 |
Aerotech E15W | 8.77 | 8:1 | 15:1 | 381.90 | 236.72 | 1.5 | 2.70 | 6.30 | 8.80 | 1413 |
Aerotech E18W | 9.01 | 9:1 | 16:1 | 401.15 | 253.07 | 1.4 | 2.30 | 6.30 | 8.40 | 1369 |
Aerotech E20W | 8.73 | 10:1 | 18:1 | 458.85 | 238.46 | 1.3 | 1.84 | 6.20 | 7.84 | 1184 |
Aerotech D21T | 7.88 | 11:1 | 17:1 | 460.73 | 159.59 | 1.3 | 0.99 | 5.20 | 5.99 | 631 |
Aerotech D24T | 8.09 | 11:1 | 21:1 | 348.71 | 129.43 | 1.7 | 0.91 | 4.70 | 5.41 | 471 |
CTI 24E22-13A | 8.99 | 11:1 | 16:1 | 398.35 | 185.02 | 1.8 | 1.10 | 5.80 | 6.70 | 788 |
Aerotech F24 | 9.20 | 11:1 | 21:1 | 513.46 | 286.99 | 1.4 | 2.21 | 6.80 | 8.81 | 1575 |
Aerotech E25T | 7.71 | 12:1 | 23:1 | 671.83 | 194.67 | 1.0 | 0.95 | 5.80 | 6.55 | 801 |
CTI 26E31-15A | 8.83 | 15:1 | 23:1 | 583.53 | 206.04 | 1.4 | 0.88 | 6.10 | 6.78 | 855 |
Aerotech E30T | 8.53 | 17:1 | 25:1 | 681.15 | 296.62 | 0.9 | 1.25 | 6.90 | 7.95 | 1337 |
Aerotech E28T | 8.92 | 17:1 | 26:1 | 649.90 | 284.19 | 1.0 | 1.26 | 6.90 | 7.96 | 1312 |
Estes E30T | 8.51 | 17:1 | 25:1 | 691.86 | 249.18 | 1.0 | 1.05 | 6.50 | 7.35 | 1077 |
Aerotech F39 | 9.11 | 19:1 | 31:1 | 778.96 | 343.25 | 0.9 | 1.35 | 7.30 | 8.45 | 1598 |
Aerotech F44W | 8.69 | 22:1 | 34:1 | 899.73 | 336.11 | 1.2 | 1.01 | 7.10 | 7.91 | 1374 |
Aerotech E50 | 8.35 | 27:1 | 28:1 | 756.89 | 345.53 | 1.0 | 0.87 | 7.20 | 7.87 | 1373 |
CTI 25E75-17A | 8.83 | 38:1 | 49:1 | 1298.89 | 175.93 | 0.7 | 0.33 | 5.70 | 5.83 | 629 |
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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