H125W Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
330 mm |
330 mm |
= |
| Prop. Weight |
188 g |
188 g |
= |
| Total Weight |
323 g |
323 g |
= |
| Avg. Thrust |
122.9 N |
125.0 N |
−2% |
| Max. Thrust |
276.0 N |
307.0 N |
−10% |
| Total Impulse |
316.8 Ns |
299.4 Ns |
+6% |
| Burn Time |
2.6 s |
2.6 s |
−1% |
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Raw Data
; AeroTech H125W
; converted from TMT test stand data 1997 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
H125W 29 330 14 0.18816 0.32256 AT
0.053 275.994
0.161 241.473
0.270 216.283
0.378 199.482
0.488 188.758
0.597 182.349
0.705 175.862
0.814 169.365
0.922 162.281
1.031 154.276
1.141 143.915
1.249 133.480
1.357 123.007
1.466 113.058
1.575 101.801
1.684 88.423
1.793 73.530
1.901 60.425
2.009 46.643
2.119 36.785
2.228 29.546
2.336 23.641
2.445 18.794
2.553 14.728
2.663 10.970
2.772 0.000
You can also download the raw data points as a CSV file.
