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; AeroTech H73J ; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) H73J 38 152 6 0.14784 0.30912 AT 0.056 49.252 0.172 82.004 0

; AeroTech N2000W ; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) N2000W 98 1046 0 7.66707 12.2828 AT 0.146 2775.075 0.446 2831.

; AeroTech H97J ; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) H97J 29 238 6 0.1344 0.27776 AT 0.045 89.405 0.136 100.289 0

; AeroTech H55W ; Copyright Tripoli Motor Testing 1998 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) H55W 29 191 0 0.09856 0.18816 AT 0.052 92.752 0.159 98.019 0

; AeroTech H70W ; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) H70W 29 229 0 0.11648 0.224 AT 0.055 114.847 0.169 131.427 0

; Kosdon I560 ; Copyright Tripoli Motor Testing 1993 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) I560 29 597 0 0.2464 0.52864 KO 0.015 589.548 0.046 867.329 0.

; Kosdon L850 ; Copyright Tripoli Motor Testing 1993 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) L850 54 727 0 1.25888 2.4416 KO 0.063 793.031 0.190 864.808 0.

; Kosdon J280 ; Copyright Tripoli Motor Testing 1993 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) J280 38 368 0 0.3136 0.70784 KO 0.047 267.342 0.144 323.238 0.

; Kosdon H155 ; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) H155 29 203 0 0.08064 0.21504 KO 0.020 57.690 0.061 124.837 0.

; Kosdon I385 ; Copyright Tripoli Motor Testing 1997 (www.tripoli.org) ; provided by ThrustCurve.org (www.thrustcurve.org) I385 29 384 0 0.15232 0.3584 KO 0.016 206.631 0.050 369.959 0.