+++ /dev/null
-; AeroTech I285R\r
-; provided by ThrustCurve.org (www.thrustcurve.org)\r
-I285R 38 250 0 0.25088 0.4928 AT\r
- 0.027 171.405\r
- 0.088 325.573\r
- 0.148 341.697\r
- 0.208 358.916\r
- 0.268 373.706\r
- 0.327 373.966\r
- 0.388 368.442\r
- 0.448 367.497\r
- 0.507 361.900\r
- 0.568 351.928\r
- 0.628 346.109\r
- 0.687 340.993\r
- 0.749 329.382\r
- 0.810 321.625\r
- 0.870 310.856\r
- 0.930 295.955\r
- 0.990 283.704\r
- 1.050 269.655\r
- 1.110 253.419\r
- 1.170 240.222\r
- 1.230 224.116\r
- 1.290 204.118\r
- 1.350 118.730\r
- 1.410 23.483\r
- 1.471 2.046\r
- 1.532 0.000\r