Rocket Motor Guide
Rocket Development Corporation Rawhide
Rocket Development Corporation - Rawhide {Kit} (F3) [1963-1969]
| 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 | 0.54 | 3:1 | 9:1 | 241.32 | 26.05 | 8.7 | 0.86 | 1.20 | 1.86 | 38 |
| Quest Micro Maxx II | 0.54 | 3:1 | 23:1 | 674.11 | 28.06 | 1.8 | 0.70 | 1.30 | 1.80 | 42 |
| Apogee A2 | 0.74 | 14:1 | 35:1 | 805.34 | 194.88 | 1.0 | 1.40 | 4.30 | 5.50 | 613 |
| Apogee 1/2A2 | 0.66 | 14:1 | 29:1 | 704.45 | 125.80 | 1.1 | 0.70 | 3.60 | 4.10 | 313 |
| Estes A3T | 0.80 | 16:1 | 42:1 | 738.90 | 171.15 | 1.1 | 1.02 | 4.30 | 5.12 | 500 |
| Estes A10T | 0.68 | 17:1 | 91:1 | 1764.20 | 177.88 | 1.0 | 0.89 | 4.00 | 4.69 | 501 |
| Estes 1/4A3T | 0.72 | 17:1 | 36:1 | 655.29 | 34.16 | 1.2 | 0.31 | 1.50 | 1.61 | 39 |
| Apogee 1/4A2 | 0.63 | 18:1 | 39:1 | 915.29 | 44.10 | 1.0 | 0.29 | 1.90 | 1.99 | 60 |
| MPC 1/2A3-M | 0.73 | 22:1 | 36:1 | 675.27 | 94.00 | 1.4 | 0.52 | 3.20 | 3.52 | 217 |
| Estes 1/2A3T | 0.73 | 22:1 | 55:1 | 838.60 | 76.86 | 1.0 | 0.39 | 2.80 | 2.99 | 155 |
| Quest C6 | 1.36 | 23:1 | 111:1 | 1589.49 | 289.71 | 1.6 | 2.54 | 5.90 | 8.24 | 1631 |
| Estes A8 | 1.08 | 23:1 | 70:1 | 922.50 | 145.57 | 1.3 | 0.74 | 4.40 | 4.94 | 450 |
| Estes 1/2A6 | 0.99 | 25:1 | 56:1 | 790.50 | 74.24 | 1.4 | 0.35 | 2.90 | 3.05 | 150 |
| Apogee C4 | 1.10 | 27:1 | 81:1 | 1249.26 | 301.77 | 0.9 | 2.36 | 5.60 | 7.76 | 1615 |
| Estes C5 | 1.25 | 28:1 | 147:1 | 2443.84 | 367.70 | 1.0 | 2.09 | 5.60 | 7.49 | 1647 |
| Estes B4 | 1.17 | 30:1 | 92:1 | 931.35 | 243.61 | 1.0 | 1.09 | 5.40 | 6.29 | 844 |
| Weco C6 | 1.24 | 34:1 | 89:1 | 1534.88 | 301.14 | 1.1 | 1.79 | 5.40 | 6.99 | 1237 |
| Estes C6 | 1.32 | 34:1 | 101:1 | 1460.83 | 377.33 | 1.1 | 1.91 | 5.90 | 7.61 | 1575 |
| Estes B6 | 1.14 | 36:1 | 87:1 | 1177.55 | 262.45 | 1.1 | 0.91 | 5.40 | 6.11 | 851 |
| Quest A6 | 1.04 | 36:1 | 85:1 | 1392.36 | 149.84 | 1.2 | 0.50 | 4.40 | 4.70 | 414 |
| Quest A8 Q-Jet | 0.96 | 37:1 | 80:1 | 1289.42 | 151.44 | 1.3 | 0.42 | 4.20 | 4.42 | 375 |
| FSI A6 | 1.07 | 39:1 | 82:1 | 1310.01 | 109.54 | 1.1 | 0.49 | 3.60 | 3.89 | 269 |
| Aerotech C6W | 1.31 | 43:1 | 85:1 | 1142.13 | 424.76 | 1.1 | 1.69 | 6.20 | 7.69 | 1597 |
| Quest B6 | 1.07 | 45:1 | 103:1 | 1882.64 | 334.06 | 1.1 | 0.78 | 5.50 | 6.08 | 945 |
| Apogee B7 | 0.82 | 48:1 | 106:1 | 1979.36 | 357.77 | 0.7 | 0.83 | 5.10 | 5.73 | 914 |
| Aerotech D8 | 1.17 | 51:1 | 110:1 | 1972.91 | 638.87 | 0.7 | 2.44 | 5.60 | 7.84 | 2368 |
| Apogee C10 | 1.12 | 72:1 | 185:1 | 2579.18 | 475.05 | 0.5 | 1.03 | 6.00 | 6.83 | 1402 |
| Aerotech C12T | 1.27 | 77:1 | 148:1 | 1998.49 | 457.14 | 0.9 | 0.96 | 6.50 | 7.26 | 1466 |
| Aerotech D13W | 1.66 | 81:1 | 160:1 | 1919.61 | 627.53 | 0.5 | 1.72 | 7.00 | 8.52 | 2331 |
| Aerotech D10W | 1.41 | 90:1 | 180:1 | 2614.24 | 693.50 | 0.4 | 1.42 | 6.60 | 7.82 | 2175 |
| Apogee D10 | 1.41 | 96:1 | 181:1 | 2688.25 | 702.73 | 0.5 | 1.42 | 6.60 | 7.82 | 2190 |
| Aerotech D21T | 1.38 | 150:1 | 231:1 | 3341.64 | 812.68 | 0.5 | 1.03 | 6.70 | 7.53 | 2078 |
| Aerotech D24T | 1.59 | 156:1 | 297:1 | 1980.45 | 662.09 | 0.6 | 0.93 | 7.30 | 8.03 | 2024 |
| Aerotech E25T | 1.21 | 167:1 | 320:1 | 5575.04 | 980.76 | 0.4 | 1.01 | 6.00 | 6.81 | 2066 |
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.
Sponsored Ads
 |
 |