H112J Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
38 mm |
38 mm |
= |
| Length |
202 mm |
191 mm |
+6% |
| Prop. Weight |
188 g |
191 g |
−2% |
| Total Weight |
379 g |
379 g |
= |
| Avg. Thrust |
85.5 N |
112.0 N |
−24% |
| Max. Thrust |
104.9 N |
121.7 N |
−14% |
| Total Impulse |
260.7 Ns |
261.1 Ns |
= |
| Burn Time |
3.0 s |
2.9 s |
+4% |
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Data Graph
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Raw Data
; AeroTech H112J
; converted from TMT test stand data 1999 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
H112J 38 202 6-10 0.187712 0.379456 AT
0.064 85.431
0.194 101.938
0.324 101.897
0.454 102.839
0.584 104.479
0.715 103.845
0.845 103.439
0.975 104.286
1.106 104.922
1.236 104.390
1.367 102.768
1.497 102.237
1.627 100.032
1.757 98.345
1.888 94.560
2.018 89.018
2.148 82.857
2.279 77.685
2.409 72.373
2.540 67.041
2.670 59.764
2.800 37.616
2.930 14.457
3.060 4.642
3.192 1.818
3.323 0.000
You can also download the raw data points as a CSV file.
