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; AeroTech H242T ; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) H242T 38 152 10 0.11648 0.2688 AT 0.030 164.060 0.093 197.516

; AeroTech K1050W ; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) K1050W 54 676 0 1.34714 2.12845 AT 0.049 1305.649 0.149 1270.3

; AeroTech J90W ; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) J90W 54 243 0 0.427392 0.852544 AT 0.143 116.187 0.430 165.444

; AeroTech K550W ; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) K550W 54 410 0 0.919744 1.48736 AT 0.065 604.264 0.196 642.625

; AeroTech L952W ; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) L952W 98 427 0 2.73011 5.01222 AT 0.141 679.073 0.425 801.562

; AeroTech K458W ; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) K458W 98 275 0 1.42778 3.16378 AT 0.133 294.911 0.403 404.808

; AeroTech I65W ; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) I65W 54 235 0 0.41216 0.7616 AT 0.180 125.414 0.544 139.304

; AeroTech J800T ; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) J800T 54 314 0 0.613312 1.08595 AT 0.040 841.341 0.121 818.497

; AeroTech J145H ; Copyright Tripoli Motor Testing 1999 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) J145H 54 709 0 0.410816 1.79738 AT 0.113 253.118 0.340 293.672

/* * v_Attract_va.java */ package EDU.gatech.cc.is.clay; import java.lang.*; import EDU.gatech.cc.is.util.Vec2; import EDU.gatech.cc.is.util.Units; /** * This node (motor schema) generates a vec