H55W Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
191 mm |
191 mm |
= |
| Prop. Weight |
99 g |
100 g |
−1% |
| Total Weight |
188 g |
188 g |
= |
| Avg. Thrust |
62.5 N |
55.0 N |
+14% |
| Max. Thrust |
98.0 N |
113.3 N |
−13% |
| Total Impulse |
161.2 Ns |
162.3 Ns |
−1% |
| Burn Time |
2.6 s |
2.5 s |
+5% |
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Data Graph
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Raw Data
; AeroTech H55W
; converted from TMT test stand data 1998 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
H55W 29 191 0 0.09856 0.18816 AT
0.052 92.752
0.159 98.019
0.268 95.821
0.375 96.162
0.482 97.146
0.591 96.927
0.699 95.915
0.806 94.447
0.914 92.001
1.022 88.756
1.129 86.970
1.236 84.072
1.345 80.172
1.453 74.343
1.560 64.990
1.668 46.380
1.776 32.835
1.883 25.734
1.991 19.920
2.099 16.229
2.207 13.059
2.315 10.451
2.422 7.700
2.530 5.696
2.639 3.979
2.747 0.000
You can also download the raw data points as a CSV file.
