Rocket Motor Guide

Enter the name of the rocket. You can optionally select a rocket from the list that may appear as you type.
Enter the diameter of the rocket's body.
Enter the weight of the rocket without the motor.
Enter the diameter of the rocket's motor mount. This sets the largest diameter motor which will fit.
Enter the length of the rocket's motor mount. This sets the longest motor which will fit.
Select the approximate drag of the rocket. Sleeker rockets with a smooth finish will have lower drag.

Rocketarium Toxic Typhoon

Rocketarium - Toxic Typhoon {Kit} (RK-TXCTN) [2012-]

MotorWeight
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 A21.545:113:1341.6324.014.51.360.601.7643
Apogee 1/2A21.465:111:1279.9823.815.00.690.601.0919
Estes A3T1.606:116:1385.2024.981.71.070.601.4734
Estes A10T1.497:135:1642.8420.421.20.930.501.2322
Estes 1/4A3T1.527:114:1319.9820.162.10.280.600.686
Apogee 1/4A21.437:115:1382.7220.192.20.260.500.566
MPC B3-M1.667:114:1299.3428.392.01.890.502.1966
MPC A3-M1.568:114:1299.3428.362.00.990.501.2929
MPC 1/2A3-M1.538:114:1292.7725.862.10.490.600.8913
Estes 1/2A3T1.538:121:1501.0224.301.30.430.600.8312
Quest C62.169:143:1735.5870.522.02.590.602.99113
Estes A81.889:127:1427.9129.341.60.780.601.1826
Estes 1/2A61.799:122:1374.0420.181.80.400.600.808
Apogee C41.9010:131:1517.8965.131.32.390.602.79113
Estes C52.0511:156:11287.47108.001.2-1.001.420.2215
Estes B41.9712:135:1661.4536.131.21.120.601.5249
Weco C62.0413:134:1535.6756.911.51.730.602.1381
Estes C62.1213:139:1554.2944.471.41.940.702.44104
Estes B61.9414:134:1507.9445.911.40.940.601.3446
Quest A61.8414:133:1438.3046.221.60.450.700.9519
Quest A8 Q-Jet1.7614:131:1675.1766.191.70.470.400.6715
Aerotech E6RCT3.1615:133:1482.58158.111.5-1.004.590.5915
Aerotech E7RCT3.0115:132:1467.45155.861.6-1.004.600.6018
FSI A61.8715:132:1563.1358.561.40.530.400.7316
Aerotech C6W2.1117:133:1580.6867.601.41.620.602.0296
Quest B61.8717:140:1509.7053.781.40.820.601.2246
Aerotech D7T2.7918:130:1442.0361.771.42.920.703.42190
Apogee B71.6219:141:1794.3474.591.20.770.601.1745
Aerotech D81.9720:142:1919.2382.980.92.460.602.86173
Aerotech E102.7223:154:1897.9685.501.24.100.504.40326
QUEST D817.3224:180:1165.6227.064.12.201.103.1082
Estes D112.8826:172:11159.0199.221.41.930.702.43152
Apogee C101.9228:171:11636.3693.520.61.040.601.4475
Aerotech D9W2.9628:155:1373.3785.772.61.940.702.44146
Estes D122.8028:182:11226.69103.831.41.730.702.23138
Aerotech C12T2.0730:157:11046.4791.971.10.980.701.4874
Estes C112.5530:160:1950.0085.121.50.840.801.4468
Aerotech E12RCJ3.4031:151:1776.5980.170.93.070.703.57269
Aerotech D13W2.4731:162:11180.7096.830.61.730.502.03140
Aerotech E11J3.5032:153:1718.0085.781.12.890.603.29249
B14T Q-Jet1.9333:148:1977.3687.150.90.470.700.9735
Aerotech D10W2.2235:169:11485.7999.310.61.430.601.83132
Apogee D102.2237:169:11512.3699.410.61.430.601.83132
Aerotech D15T2.8539:179:11189.98101.770.71.430.701.93131
Aerotech F123.6541:165:1938.2593.450.82.950.603.35292
Aerotech E15W3.0742:180:11257.29100.750.72.740.603.14275
Aerotech E18W3.3150:186:11321.76108.590.72.240.702.74242
Aerotech E20W3.0355:196:11531.29124.910.71.790.702.29199
Aerotech D21T2.1858:189:11956.62142.350.51.030.601.43100
Aerotech D24T2.4060:1114:11261.8197.470.70.940.701.44105
CTI 24E22-13A3.2961:185:11290.00102.670.71.130.801.73141
Aerotech F243.5161:1113:11581.49128.240.92.160.802.76261
Aerotech E25T2.0164:1123:12914.42189.680.4-1.001.320.1214
CTI 26E31-15A3.1481:1121:11946.12117.780.50.930.801.53130
Aerotech E30T2.8390:1133:12428.53186.120.51.220.801.82157
Aerotech E28T3.2290:1140:12104.32164.230.51.220.801.82181
Estes E30T2.8191:1136:12572.43171.170.51.120.601.52139
Aerotech F393.42103:1164:12467.74189.190.51.420.802.02205
Aerotech F44W2.99118:1180:13023.07226.980.8-1.001.360.1632
Aerotech E502.66144:1152:12722.57206.590.6-1.001.330.1326
CTI 25E75-17A3.14205:1263:14209.24271.130.4-1.001.310.1132

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.