H14ST Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
240 mm |
240 mm |
= |
| Prop. Weight |
134 g |
134 g |
= |
| Total Weight |
230 g |
230 g |
= |
| Avg. Thrust |
13.5 N |
13.2 N |
+2% |
| Max. Thrust |
40.2 N |
42.1 N |
−4% |
| Total Impulse |
242.5 Ns |
240.1 Ns |
+1% |
| Burn Time |
17.9 s |
18.3 s |
−2% |
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Data Graph
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Raw Data
; AeroTech H14ST-P
; from Tripoli Motor Testing Motor Certification Data
; created by Alexander Unmack 09/05/2023
H14ST-P 29 240 P 0.134 0.23 AT
0.045 32.284
0.253 37.105
0.343 40.246
0.417 19.502
0.625 16.946
1.787 14.535
3.946 13.659
7.029 13.001
11.839 12.782
15.443 12.344
16.366 12.052
16.515 11.76
16.575 10.664
16.828 10.956
17.23 11.321
17.587 12.198
17.736 10.591
17.96 0.0
You can also download the raw data points as a CSV file.