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| Rocket Name: | Prochron S1_0811B | Owner: | Terry Wilson |
|---|---|---|
| Body Diameter: | 100.0mm | |
| Dry Weight: | 68.000Kg | |
| MMT Diameter: | 98.0mm | |
| MMT Length: | 1,500.0mm | |
| CD: | 0.60 | |
| Web Site: | http://ascentroadmap.blogspot.com/2008/11/prochron-0811b.html |
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 L3150 | 72.731Kg | 21m/s | 52m/s | 4.1G | 179m | 6.8s | 5s |
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Cesaroni M2505 | 74.250Kg | 18m/s | 73m/s | 3.1G | 378m | 10.3s | 7s |
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AeroTech M2100 | 74.918Kg | 16m/s | 70m/s | 3.1G | 387m | 10.6s | 7s |
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AeroTech M2400 | 74.451Kg | 17m/s | 73m/s | 2.8G | 393m | 10.6s | 7s |
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AeroTech M1845 | 74.682Kg | 15m/s | 69m/s | 2.4G | 409m | 11.2s | 6s |
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Cesaroni M4770 | 74.503Kg | 26m/s | 86m/s | 7.0G | 436m | 10.2s | 9s |
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AeroTech M2000 | 76.987Kg | 15m/s | 79m/s | 2.2G | 498m | 12.4s | 8s |
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AeroTech M2500 | 76.064Kg | 18m/s | 92m/s | 2.9G | 609m | 13.0s | 9s |
W |
AMW N2020 | 77.969Kg | 16m/s | 87m/s | 2.7G | 616m | 13.5s | 9s |
W |
AMW N2600 | 78.473Kg | 16m/s | 99m/s | 3.5G | 687m | 13.9s | 10s |
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Cesaroni M3400 | 76.108Kg | 21m/s | 106m/s | 4.3G | 719m | 13.5s | 11s |
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Cesaroni N2600 | 79.482Kg | 17m/s | 103m/s | 3.0G | 755m | 14.6s | 10s |
W |
AMW N2700 | 77.931Kg | 18m/s | 110m/s | 3.7G | 837m | 15.0s | 11s |
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Cesaroni N10000 | 77.918Kg | 41m/s | 127m/s | 14.5G | 857m | 13.7s | 13s |
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Cesaroni N1100 | 79.589Kg | 16m/s | 79m/s | 2.5G | 895m | 18.3s | 6s |
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AeroTech N2000 | 80.283Kg | 18m/s | 107m/s | 2.8G | 997m | 17.1s | 9s |
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Loki N3800 | 79.600Kg | 24m/s | 130m/s | 5.6G | 1,079m | 16.2s | 13s |
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Cesaroni N2500 | 79.668Kg | 20m/s | 124m/s | 3.7G | 1,152m | 17.7s | 12s |
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AeroTech N3300 | 80.054Kg | 17m/s | 136m/s | 4.6G | 1,179m | 17.6s | 13s |
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Cesaroni N2850 | 79.688Kg | 19m/s | 132m/s | 3.4G | 1,195m | 17.9s | 13s |
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Cesaroni N3400 | 81.972Kg | 19m/s | 141m/s | 4.2G | 1,280m | 18.2s | 14s |
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Cesaroni N3180 | 80.198Kg | 20m/s | 141m/s | 3.9G | 1,308m | 18.5s | 14s |
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AMW N2800 | 81.809Kg | 20m/s | 136m/s | 3.7G | 1,332m | 18.7s | 13s |
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AMW N4000 | 81.668Kg | 25m/s | 166m/s | 5.8G | 1,729m | 20.3s | 16s |
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Cesaroni N2900 | 82.166Kg | 21m/s | 164m/s | 4.0G | 1,881m | 22.1s | 16s |
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Cesaroni N3800 | 82.261Kg | 23m/s | 176m/s | 5.1G | 1,957m | 21.8s | 17s |
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Cesaroni N4100 | 82.748Kg | 23m/s | 183m/s | 5.1G | 2,000m | 22.1s | 18s |
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AeroTech N4800 | 82.784Kg | 27m/s | 196m/s | 6.3G | 2,337m | 23.6s | 18s |
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Cesaroni N5800 | 82.826Kg | 29m/s | 221m/s | 7.9G | 2,714m | 24.7s | 21s |
W Motor total weight unknown, lift-off Weight not accurate.
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 | |
|---|---|---|
5 |
AeroTech K680 | average thrust fails 5:1 thrust/weight ratio (1:1) |
5 |
AeroTech K650 | average thrust fails 5:1 thrust/weight ratio (1:1) |
G |
Cesaroni K1620 | speed at end of launch guide too slow (14m/s) |
5 |
AeroTech K458 | average thrust fails 5:1 thrust/weight ratio (1:1) |
A |
AeroTech K1999 | rocket doesn't reach a safe altitude (41m) |
5 |
AeroTech L339 | average thrust fails 5:1 thrust/weight ratio (0:1) |
G |
AeroTech L1300 | speed at end of launch guide too slow (11m/s) |
5 |
AeroTech L400 | average thrust fails 5:1 thrust/weight ratio (1:1) |
G |
AeroTech L952 | speed at end of launch guide too slow (7m/s) |
G |
Cesaroni L610 | speed at end of launch guide too slow (4m/s) |
G |
AeroTech L1500 | speed at end of launch guide too slow (13m/s) |
G |
Cesaroni M1560 | speed at end of launch guide too slow (12m/s) |
G |
AeroTech M845 | speed at end of launch guide too slow (9m/s) |
G |
Hypertek M1015 | speed at end of launch guide too slow (11m/s) |
G |
Hypertek M956 | speed at end of launch guide too slow (10m/s) |
G |
AeroTech M1600 | speed at end of launch guide too slow (13m/s) |
G |
Cesaroni M520 | speed at end of launch guide too slow (5m/s) |
G |
Cesaroni M1060 | speed at end of launch guide too slow (11m/s) |
G |
Cesaroni M1520 | speed at end of launch guide too slow (13m/s) |
G |
AeroTech M1419 | speed at end of launch guide too slow (10m/s) |
G |
Cesaroni M1790 | speed at end of launch guide too slow (13m/s) |
G |
AMW M1730 | speed at end of launch guide too slow (12m/s) |
G |
AeroTech M1800 | speed at end of launch guide too slow (14m/s) |
G |
Hypertek M1010 | speed at end of launch guide too slow (11m/s) |
G |
Hypertek M1000 | speed at end of launch guide too slow (11m/s) |
G |
AeroTech M750 | speed at end of launch guide too slow (8m/s) |
G |
Hypertek M1001 | speed at end of launch guide too slow (10m/s) |
G |
Cesaroni M1800 | speed at end of launch guide too slow (14m/s) |
G |
Cesaroni M1890 | speed at end of launch guide too slow (14m/s) |
G |
Cesaroni M1450 | speed at end of launch guide too slow (14m/s) |
G |
Hypertek M1040 | speed at end of launch guide too slow (10m/s) |
G |
Cesaroni M795 | speed at end of launch guide too slow (10m/s) |
G |
AeroTech M1939 | speed at end of launch guide too slow (14m/s) |
5 |
AMW N2801 | average thrust fails 5:1 thrust/weight ratio (3:1) |
G |
AeroTech N1000 | speed at end of launch guide too slow (12m/s) |
G |
Cesaroni N1975 | speed at end of launch guide too slow (12m/s) |
G These simulations were run with a launch guide length of 6m (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.
A The minimum altitude check is used to ensure that the rocket flies high enough to ensure time for a safe recovery. In addition, many barometric altimeters require a minimum altitude to detect lift-off. (The minimum altitude is 10m or 33ft for an A motor and doubles for each impulse class).
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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