J125W Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
54 mm |
54 mm |
= |
| Length |
368 mm |
368 mm |
= |
| Prop. Weight |
634 g |
639 g |
−1% |
| Total Weight |
1,288 g |
1,288 g |
= |
| Avg. Thrust |
139.7 N |
125.0 N |
+12% |
| Max. Thrust |
285.2 N |
338.9 N |
−16% |
| Total Impulse |
1,204.4 Ns |
1,202.4 Ns |
= |
| Burn Time |
8.6 s |
7.8 s |
+11% |
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Data Graph
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Raw Data
; AeroTech J125
; converted from TMT test stand data 1997 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
J125 54 368 0 0.63392 1.288 AT
0.174 223.931
0.525 254.842
0.877 275.347
1.229 285.163
1.581 280.333
1.933 264.476
2.285 244.373
2.638 223.774
2.990 204.720
3.342 185.434
3.694 166.807
4.046 147.653
4.398 127.914
4.750 108.483
5.102 92.582
5.454 77.817
5.806 63.844
6.158 53.017
6.510 44.507
6.862 37.543
7.215 32.205
7.567 27.212
7.919 22.847
8.271 18.596
8.623 14.790
8.975 0.000
You can also download the raw data points as a CSV file.
