M1939W Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
98 mm |
98 mm |
= |
| Length |
732 mm |
732 mm |
= |
| Prop. Weight |
5,656 g |
5,719 g |
−1% |
| Total Weight |
8,988 g |
8,988 g |
= |
| Avg. Thrust |
1,664.8 N |
1,939.0 N |
−14% |
| Max. Thrust |
2,229.9 N |
2,429.7 N |
−8% |
| Total Impulse |
10,368.6 Ns |
10,481.5 Ns |
−1% |
| Burn Time |
6.2 s |
6.2 s |
= |
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Raw Data
; AeroTech M1939W
; converted from TMT test stand data 1998 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
M1939W 98 732 0 5.656 8.98822 AT
0.134 1905.185
0.406 2021.155
0.679 2095.900
0.952 2158.087
1.225 2198.211
1.498 2219.694
1.770 2228.643
2.042 2229.881
2.315 2225.641
2.587 2211.713
2.860 2164.724
3.133 2047.014
3.405 1916.238
3.677 1805.664
3.950 1658.489
4.223 1497.704
4.496 1339.452
4.769 1213.061
5.041 1102.130
5.313 966.508
5.585 670.253
5.858 443.975
6.131 155.355
6.404 41.358
6.677 5.775
6.950 0.000
You can also download the raw data points as a CSV file.
