I200W Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
333 mm |
333 mm |
= |
| Prop. Weight |
182 g |
187 g |
−3% |
| Total Weight |
358 g |
358 g |
= |
| Avg. Thrust |
188.7 N |
200.0 N |
−6% |
| Max. Thrust |
304.0 N |
463.3 N |
−34% |
| Total Impulse |
326.8 Ns |
324.5 Ns |
+1% |
| Burn Time |
1.7 s |
1.7 s |
+5% |
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Data Graph
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Raw Data
; AeroTech I200W
; converted from TMT test stand data 1999 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
I200W 29 333 0 0.181888 0.357504 AT
0.033 303.951
0.103 273.452
0.174 276.061
0.245 271.625
0.316 268.233
0.386 258.449
0.457 252.480
0.528 246.642
0.599 242.304
0.670 237.737
0.741 234.769
0.811 233.171
0.882 230.660
0.953 224.985
1.024 221.658
1.095 214.548
1.166 177.365
1.236 154.208
1.307 119.146
1.378 91.586
1.449 65.330
1.520 32.877
1.591 28.702
1.661 22.211
1.732 15.558
1.803 0.000
You can also download the raw data points as a CSV file.
