L2525-GF Data (RASP)
Accuracy of this data file:
| |
This File |
Certified |
± |
| Diameter |
76 mm |
75 mm |
+1% |
| Length |
1,524 mm |
1,524 mm |
= |
| Prop. Weight |
1,306 g |
1,306 g |
= |
| Total Weight |
5,579 g |
5,579 g |
= |
| Avg. Thrust |
2,468.0 N |
2,456.0 N |
= |
| Max. Thrust |
4,905.8 N |
4,905.8 N |
= |
| Total Impulse |
4,676.5 Ns |
4,677.0 Ns |
= |
| Burn Time |
1.9 s |
1.9 s |
= |
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Data Graph
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Raw Data
; Contrail L2525GF Hybrid Rocket Motor
; from Tripoli Motor Testing Motor Certification Data
; created by Alexander Unmack 09/05/2023
L2525GF-P 76 1524 P 1.306 5.579 Contrail
0.014 2794.513
0.028 3183.154
0.042 1943.205
0.082 4339.824
0.099 4885.772
0.131 4905.845
0.159 1859.924
0.199 1721.124
0.237 1767.391
0.27 3432.995
0.422 4256.543
0.541 4265.797
0.632 4089.983
0.821 2961.074
0.891 3164.647
1.142 2294.832
1.163 2017.231
1.768 508.935
1.895 314.614
1.900 0.0
You can also download the raw data points as a CSV file.
