H210R Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
29 mm |
29 mm |
= |
| Length |
238 mm |
238 mm |
= |
| Prop. Weight |
121 g |
106 g |
+14% |
| Total Weight |
246 g |
246 g |
= |
| Avg. Thrust |
214.0 N |
215.4 N |
−1% |
| Max. Thrust |
260.2 N |
275.7 N |
−6% |
| Total Impulse |
210.6 Ns |
215.4 Ns |
−2% |
| Burn Time |
1.0 s |
1.0 s |
−2% |
Add this file to my outbox.
Data Graph
File Notes
Do you have a comment on this file?
Please add a note.
Raw Data
; AeroTech H210R
; provided by ThrustCurve.org (www.thrustcurve.org)
H210R 29 238 14-10-6 0.12096 0.2464 AT
0.019 105.923
0.059 211.290
0.099 219.770
0.139 229.639
0.179 235.082
0.220 241.594
0.260 242.706
0.300 245.347
0.341 249.100
0.381 253.410
0.421 258.553
0.461 260.221
0.502 257.997
0.543 259.248
0.583 256.607
0.623 252.436
0.663 245.056
0.704 219.909
0.744 209.344
0.784 200.587
0.824 193.565
0.865 184.323
0.905 153.881
0.945 58.244
0.986 13.210
1.027 0.000
You can also download the raw data points as a CSV file.
