H123W Data (RASP)
Accuracy of this data file:
|
This File |
Certified |
± |
Diameter |
38 mm |
38 mm |
= |
Length |
154 mm |
152 mm |
+1% |
Prop. Weight |
126 g |
129 g |
−2% |
Total Weight |
279 g |
275 g |
+1% |
Avg. Thrust |
104.6 N |
123.0 N |
−15% |
Max. Thrust |
152.5 N |
174.2 N |
−12% |
Total Impulse |
235.2 Ns |
223.6 Ns |
+5% |
Burn Time |
2.2 s |
1.8 s |
+28% |
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Raw Data
; AeroTech H123W
; converted from TMT test stand data 1999 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
H123W 38 154 0 0.126336 0.278656 AT
0.047 96.764
0.143 146.256
0.239 150.699
0.334 152.496
0.430 151.248
0.526 149.875
0.622 150.200
0.718 149.176
0.814 144.858
0.909 143.536
1.005 141.414
1.101 135.125
1.198 125.288
1.295 114.035
1.391 101.556
1.486 90.175
1.582 78.694
1.678 66.364
1.774 54.260
1.870 46.872
1.966 38.186
2.061 22.737
2.157 13.478
2.253 7.587
2.350 5.252
2.447 0.000
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