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Rocket Name: | Mega Der Red Max Clone 29mm | Owner: | Nick Hutton |
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Body Diameter: | 100.0mm | |
Dry Weight: | 1,100g | |
MMT Diameter: | 29.0mm | |
MMT Length: | 275.0mm | |
CD: | 0.90 |
These motors fit your rocket and appear to have enough thrust to lift it safely. If thrust curves are available, a quick simulation has been run to give a rough idea of the performance of your rocket on this motor. We encourage you to run a more complete simulation with any motor you plan to use; see the simulators page for more info.
Motor | Weight | Launch | Velocity | Accel | Altitude | Time | Delay | |
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Cesaroni F120 | 1,206g | 17m/s | 41m/s | 11.0G | 75m | 4.0s | 4s |
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AeroTech G104 | 1,236g | 16m/s | 57m/s | 9.0G | 136m | 5.2s | 4s |
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Cesaroni G250 | 1,241g | 23m/s | 82m/s | 22.4G | 188m | 5.8s | 5s |
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AeroTech G76 | 1,247g | 18m/s | 65m/s | 11.3G | 199m | 6.2s | 4s |
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Cesaroni G126 | 1,245g | 18m/s | 78m/s | 12.0G | 200m | 6.1s | 5s |
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AeroTech G64 | 1,251g | 15m/s | 64m/s | 7.8G | 204m | 6.4s | 4s |
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Cesaroni G131 | 1,300g | 17m/s | 82m/s | 10.6G | 212m | 6.3s | 5s |
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AeroTech G125 | 1,225g | 17m/s | 86m/s | 11.2G | 220m | 6.3s | 5s |
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AeroTech G80 | 1,228g | 15m/s | 77m/s | 7.6G | 227m | 6.6s | 5s |
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KBA G135 | 1,326g | 15m/s | 92m/s | 10.7G | 244m | 6.6s | 6s |
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AeroTech H165 | 1,302g | 19m/s | 103m/s | 13.7G | 275m | 6.8s | 6s |
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Cesaroni G125 | 1,295g | 17m/s | 98m/s | 11.7G | 276m | 7.0s | 6s |
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Cesaroni G118 | 1,288g | 16m/s | 97m/s | 11.4G | 276m | 7.0s | 6s |
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Cesaroni H175 | 1,347g | 19m/s | 107m/s | 15.0G | 280m | 6.9s | 6s |
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Cesaroni H410 | 1,283g | 30m/s | 122m/s | 39.8G | 282m | 6.6s | 6s |
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Cesaroni H133 | 1,290g | 18m/s | 100m/s | 14.2G | 283m | 7.0s | 6s |
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Cesaroni G54 | 1,293g | 15m/s | 72m/s | 8.5G | 285m | 7.6s | 5s |
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Cesaroni H163 | 1,287g | 19m/s | 107m/s | 16.2G | 287m | 6.9s | 6s |
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AeroTech G138 | 1,248g | 17m/s | 111m/s | 12.5G | 291m | 7.0s | 6s |
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Cesaroni H90 | 1,263g | 16m/s | 93m/s | 11.5G | 291m | 7.3s | 5s |
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AeroTech H128 | 1,306g | 19m/s | 105m/s | 13.1G | 294m | 7.1s | 6s |
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AeroTech H238 | 1,296g | 22m/s | 112m/s | 17.3G | 295m | 6.9s | 6s |
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Cesaroni H123 | 1,328g | 16m/s | 104m/s | 9.7G | 301m | 7.3s | 6s |
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AeroTech H115 | 1,305g | 15m/s | 102m/s | 8.5G | 307m | 7.3s | 6s |
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Cesaroni H118 | 1,332g | 17m/s | 104m/s | 12.0G | 319m | 7.4s | 6s |
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Cesaroni H237 | 1,394g | 23m/s | 130m/s | 18.7G | 336m | 7.2s | 6s |
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AeroTech H220 | 1,350g | 23m/s | 129m/s | 22.2G | 339m | 7.2s | 6s |
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AeroTech H210 | 1,346g | 21m/s | 130m/s | 17.8G | 345m | 7.3s | 6s |
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Cesaroni H151 | 1,338g | 20m/s | 119m/s | 14.5G | 347m | 7.4s | 6s |
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Cesaroni H170 | 1,332g | 21m/s | 127m/s | 17.2G | 360m | 7.5s | 6s |
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AeroTech H182 | 1,307g | 19m/s | 133m/s | 13.4G | 361m | 7.5s | 6s |
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Cesaroni H160 | 1,372g | 19m/s | 127m/s | 12.8G | 362m | 7.6s | 6s |
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Cesaroni H135 | 1,351g | 18m/s | 119m/s | 11.5G | 364m | 7.7s | 6s |
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AeroTech H180 | 1,352g | 22m/s | 133m/s | 18.0G | 370m | 7.5s | 6s |
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AeroTech H250 | 1,356g | 26m/s | 142m/s | 23.2G | 372m | 7.4s | 6s |
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AeroTech H195 | 1,297g | 23m/s | 143m/s | 19.0G | 386m | 7.6s | 6s |
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AeroTech H169 | 1,302g | 22m/s | 132m/s | 17.2G | 386m | 7.6s | 6s |
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AeroTech H135 | 1,312g | 17m/s | 119m/s | 10.9G | 389m | 8.0s | 6s |
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Cesaroni H194 | 1,384g | 22m/s | 142m/s | 19.8G | 407m | 7.8s | 6s |
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Cesaroni H200 | 1,374g | 23m/s | 145m/s | 20.5G | 414m | 7.8s | 6s |
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Cesaroni H255 | 1,332g | 26m/s | 161m/s | 27.8G | 423m | 7.7s | 7s |
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Cesaroni H140 | 1,377g | 21m/s | 133m/s | 17.2G | 434m | 8.1s | 6s |
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Estes G80 | 1,228g | 6:1 thrust/weight ratio (no data) |
D No simulation data found for this motor.
Don't like the units? Login to set your preferences. Don't understand the results? See the motor guide help page.
These motors fit your rocket, but failed one safety check or another. They may actually work, but you should use them only with caution. We encourage you to run a more complete simulation to verify flight safety; see the simulators page for more info.
Motor | Reason | |
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Estes E16 | speed at end of launch guide too slow (5m/s) |
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AeroTech E23 | speed at end of launch guide too slow (8m/s) |
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AeroTech E16 | speed at end of launch guide too slow (6m/s) |
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AeroTech F23 | speed at end of launch guide too slow (8m/s) |
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Cesaroni F36 | speed at end of launch guide too slow (8m/s) |
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AeroTech F27 | speed at end of launch guide too slow (8m/s) |
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Estes F15 | speed at end of launch guide too slow (4m/s) |
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AeroTech F37 | speed at end of launch guide too slow (9m/s) |
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AeroTech F62 | speed at end of launch guide too slow (11m/s) |
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Cesaroni F36 | speed at end of launch guide too slow (9m/s) |
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AeroTech F20 | speed at end of launch guide too slow (9m/s) |
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Cesaroni F32 | speed at end of launch guide too slow (7m/s) |
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AeroTech F42 | speed at end of launch guide too slow (12m/s) |
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Cesaroni F29 | speed at end of launch guide too slow (7m/s) |
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Cesaroni F31 | speed at end of launch guide too slow (8m/s) |
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Cesaroni F59 | speed at end of launch guide too slow (12m/s) |
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AeroTech F67 | speed at end of launch guide too slow (14m/s) |
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Estes F26 | average thrust fails 5:1 thrust/weight ratio (2:1) |
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AeroTech F26 | speed at end of launch guide too slow (8m/s) |
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AeroTech F22 | speed at end of launch guide too slow (6m/s) |
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AeroTech F52 | speed at end of launch guide too slow (13m/s) |
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Apogee F10 | speed at end of launch guide too slow (5m/s) |
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AeroTech F50 | speed at end of launch guide too slow (12m/s) |
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Estes F50 | speed at end of launch guide too slow (12m/s) |
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AeroTech F25 | speed at end of launch guide too slow (10m/s) |
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AeroTech F40 | speed at end of launch guide too slow (11m/s) |
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AeroTech G54 | speed at end of launch guide too slow (12m/s) |
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AeroTech G74 | speed at end of launch guide too slow (13m/s) |
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Cesaroni G88 | speed at end of launch guide too slow (14m/s) |
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AeroTech G38 | speed at end of launch guide too slow (9m/s) |
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AeroTech G53 | speed at end of launch guide too slow (13m/s) |
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Cesaroni G80 | speed at end of launch guide too slow (13m/s) |
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Estes G40 | speed at end of launch guide too slow (11m/s) |
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AeroTech G77 | speed at end of launch guide too slow (13m/s) |
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AeroTech G77 | speed at end of launch guide too slow (12m/s) |
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AeroTech G72 | speed at end of launch guide too slow (12m/s) |
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Cesaroni G83 | speed at end of launch guide too slow (14m/s) |
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Cesaroni G57 | speed at end of launch guide too slow (13m/s) |
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Cesaroni G68 | speed at end of launch guide too slow (12m/s) |
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AeroTech G79 | speed at end of launch guide too slow (11m/s) |
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AeroTech G79 | speed at end of launch guide too slow (13m/s) |
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AeroTech G78 | speed at end of launch guide too slow (14m/s) |
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AeroTech G40 | speed at end of launch guide too slow (11m/s) |
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AeroTech G25 | speed at end of launch guide too slow (8m/s) |
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AeroTech G75 | speed at end of launch guide too slow (14m/s) |
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AeroTech G75 | speed at end of launch guide too slow (12m/s) |
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AeroTech G8 | average thrust fails 5:1 thrust/weight ratio (1:1) |
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Cesaroni G106 | speed at end of launch guide too slow (14m/s) |
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AeroTech G11 | speed at end of launch guide too slow (5m/s) |
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AeroTech G12 | speed at end of launch guide too slow (6m/s) |
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KBA G82 | speed at end of launch guide too slow (12m/s) |
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Cesaroni G33 | speed at end of launch guide too slow (8m/s) |
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Cesaroni H54 | speed at end of launch guide too slow (14m/s) |
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Cesaroni H87 | speed at end of launch guide too slow (14m/s) |
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AeroTech H97 | speed at end of launch guide too slow (14m/s) |
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Cesaroni H42 | speed at end of launch guide too slow (10m/s) |
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Cesaroni H53 | speed at end of launch guide too slow (12m/s) |
G These simulations were run with a launch guide length of 2m (rod, rail or tower). If this is not correct, launch guide lengths can be specified for your saved rockets. (The minimum velocity required is approximately 15m/s or 50ft/s.)
5 The 5:1 thrust-to-weight ratio check is a useful rule of thumb, but it does break down for motors with unusual thrust curves. For example, motors with a high initial thrust and a long tail-off may fail this test but still be safe for use.
The data is presented in a compact form in the tables above, broken down by motors that worked and those that did not. If you would like to analyze the data further, this section provides download links for files in a generic spreadsheet format (comma-separated value, or CSV) that can be opened with almost any spreadsheet program.
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Download full details of the simulation runs with the various motors:
that worked, that failed, or all of them. |
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  | Download the list of motors that fit your rocket into a batch for use with SMARTSim. (See the Simulators page for more info.) |
You should download these files to your machine and then open them. Normally, clicking the link will prompt you to do this. However, if your browser insists on opening the file as plain text, you can right-click (control-click on the Mac) on the link and chose Save File As (or similar).
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