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.

FlisKits Adfecta

FlisKits - Adfecta {Kit} (FR010)

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 A22.144:19:1242.1657.195.11.322.203.32136
Apogee 1/2A22.064:18:1196.9530.345.30.641.301.7439
Estes A3T2.204:111:1290.8954.362.41.012.102.91115
Estes A10T2.094:124:1614.5835.811.30.951.502.2562
MPC B3-M2.265:19:1248.5896.112.71.942.804.54298
MPC A3-M2.165:19:1248.5854.222.70.942.002.74106
MPC 1/2A3-M2.136:19:1248.4427.472.50.531.201.5328
Estes 1/2A3T2.136:114:1394.0226.041.60.451.101.3526
Quest C62.766:129:1640.89117.842.02.613.405.81556
Estes A82.486:118:1413.3144.871.70.801.802.4079
Estes 1/2A62.396:115:1352.4220.131.90.420.901.1214
Apogee C42.507:121:1487.44122.601.62.413.405.61588
Estes C52.657:139:1922.25153.721.32.033.605.43603
Estes B42.578:124:1580.8488.171.31.032.903.73225
Weco C62.649:123:1429.48116.181.61.743.304.84396
Estes C62.729:127:1512.08152.651.41.953.605.35535
Estes B62.5410:123:1493.1197.001.50.963.003.76233
Quest A62.4410:122:1429.3143.561.70.461.802.0664
Quest A8 Q-Jet2.3610:121:1381.8346.261.80.391.902.0963
Aerotech E6RCT3.7610:123:1405.87192.241.67.603.5010.101920
Aerotech E7RCT3.6110:122:1397.97190.001.75.614.008.611503
FSI A62.4710:122:1442.6239.821.60.541.501.8450
Aerotech C6W2.7111:122:1493.03185.101.51.643.705.14581
Quest B62.4712:127:1493.04112.381.50.843.203.84262
Apogee E63.5312:138:1757.21205.091.26.074.009.071842
Aerotech D7T3.3912:121:1385.60194.241.62.934.206.931004
Apogee B72.2213:128:1657.81125.101.30.783.303.88299
Aerotech D82.5713:129:1726.43265.851.02.473.705.97976
Aerotech E103.3216:137:1741.19353.191.34.113.807.711712
QUEST D817.9216:155:1162.6736.504.32.221.703.72117
Estes D113.4818:149:1981.19238.861.51.944.306.04898
Apogee C102.5219:149:11234.23199.610.71.053.804.65526
Aerotech D9W3.5619:138:1582.18273.562.61.964.506.26901
Estes D123.4019:156:11063.43241.231.41.754.305.85851
Aerotech C12T2.6720:139:1823.60196.211.20.994.004.79522
Estes C113.1521:141:1814.80182.381.50.854.104.75479
Aerotech E12RCJ4.0021:135:1660.38320.401.03.084.407.281475
Aerotech D13W3.0721:142:1914.61290.940.71.744.105.64894
Aerotech E11J4.1022:136:1624.36319.141.32.904.507.201405
Aerotech D10W2.8124:147:11138.97306.590.71.434.205.43863
Apogee D102.8125:148:11145.44310.000.71.444.205.44867
Aerotech D15T3.4527:154:1991.43289.560.81.444.505.74887
Aerotech F124.2528:145:1805.63374.190.92.964.607.361649
Aerotech E15W3.6729:155:11047.64352.070.72.644.607.041565
Aerotech E18W3.9134:159:11094.51411.820.82.254.706.751460
Aerotech E20W3.6338:166:11263.11414.410.71.794.806.391283
Aerotech D21T2.7839:161:11487.96359.660.61.044.405.24832
Aerotech D24T2.9941:178:11078.00304.060.70.944.605.34776
CTI 24E22-13A3.8942:158:11085.07380.090.71.145.005.941014
Aerotech F244.1142:178:11332.70448.000.92.175.006.971615
Aerotech E25T2.6144:184:12257.86417.820.51.024.305.12890
CTI 26E31-15A3.7455:183:11582.74427.140.60.935.105.831027
Aerotech E30T3.4361:191:11930.15515.680.51.224.805.821270
Aerotech E28T3.8262:196:11738.01487.350.61.235.206.231315
Estes E30T3.4162:193:12017.66459.780.51.024.905.721128
Aerotech F394.0271:1113:12036.90539.580.51.425.206.421500
Aerotech F44W3.5980:1123:12443.10642.350.81.075.005.871265
Aerotech E503.2699:1104:12141.42625.660.60.844.905.541192
CTI 25E75-17A3.74140:1180:13437.48422.400.40.415.205.41838

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.