K560W Data (RASP)
Accuracy of this data file:
|
This File |
Certified |
± |
Diameter |
75 mm |
75 mm |
= |
Length |
396 mm |
396 mm |
= |
Prop. Weight |
1,408 g |
1,425 g |
−1% |
Total Weight |
2,714 g |
2,744 g |
−1% |
Avg. Thrust |
551.6 N |
560.0 N |
−2% |
Max. Thrust |
789.3 N |
753.7 N |
+5% |
Total Impulse |
2,467.2 Ns |
2,417.0 Ns |
+2% |
Burn Time |
4.5 s |
4.1 s |
+9% |
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Raw Data
; AeroTech K560W
; converted from TMT test stand data 1998 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
K560W 75 396 0 1.40806 2.71354 AT
0.096 552.123
0.290 645.403
0.484 681.109
0.679 716.167
0.874 742.678
1.069 764.778
1.264 775.710
1.458 785.859
1.653 789.305
1.848 789.077
2.043 744.622
2.237 676.886
2.432 614.711
2.627 557.908
2.822 503.641
3.017 455.504
3.211 412.045
3.406 372.963
3.601 335.987
3.796 307.346
3.991 279.856
4.185 223.491
4.380 70.441
4.575 10.028
4.770 2.445
4.965 0.000
You can also download the raw data points as a CSV file.