-; AeroTech H210R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-H210R 29 238 0 0.12096 0.2464 AT\r
- 0.019 105.923\r
- 0.059 211.290\r
- 0.099 219.770\r
- 0.139 229.639\r
- 0.179 235.082\r
- 0.220 241.594\r
- 0.260 242.706\r
- 0.300 245.347\r
- 0.341 249.100\r
- 0.381 253.410\r
- 0.421 258.553\r
- 0.461 260.221\r
- 0.502 257.997\r
- 0.543 259.248\r
- 0.583 256.607\r
- 0.623 252.436\r
- 0.663 245.056\r
- 0.704 219.909\r
- 0.744 209.344\r
- 0.784 200.587\r
- 0.824 193.565\r
- 0.865 184.323\r
- 0.905 153.881\r
- 0.945 58.244\r
- 0.986 13.210\r
- 1.027 0.000\r