M1419W Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
98 mm |
98 mm |
= |
| Length |
579 mm |
579 mm |
= |
| Prop. Weight |
4,032 g |
4,077 g |
−1% |
| Total Weight |
6,916 g |
6,916 g |
= |
| Avg. Thrust |
1,079.8 N |
1,419.0 N |
−24% |
| Max. Thrust |
1,513.1 N |
1,590.9 N |
−5% |
| Total Impulse |
7,674.1 Ns |
7,755.5 Ns |
−1% |
| Burn Time |
7.1 s |
7.1 s |
= |
Add this file to my outbox.
Data Graph
File Notes
Do you have a comment on this file?
Please add a note.
Raw Data
; AeroTech M1419W
; converted from TMT test stand data 1998 (www.tripoli.org)
; provided by ThrustCurve.org (www.thrustcurve.org)
M1419W 98 579 0 4.032 6.91622 AT
0.154 1154.896
0.465 1241.151
0.776 1300.224
1.087 1358.364
1.399 1411.033
1.710 1461.033
2.022 1485.747
2.333 1503.653
2.644 1513.113
2.955 1511.947
3.267 1492.438
3.578 1418.368
3.890 1326.608
4.201 1219.222
4.513 1087.648
4.824 937.068
5.135 810.066
5.446 709.130
5.757 624.701
6.069 557.223
6.380 437.806
6.692 252.076
7.003 107.741
7.315 19.973
7.626 0.515
7.937 0.000
You can also download the raw data points as a CSV file.
