Research Article
Experimental Study of the Swirling Oxidizer Flow in HTPB/N2O Hybrid Rocket Motor
Table 2
Ballistic characteristics of axial flow tests.
| Test # | (sec) | (bar) | (kgf) | (g/s) | (mm) | O/F | (m/sec) | |
| 1-S0A1 | 7.60 | 39.2 | 43.2 | 53 | 54.81 | 3.23 | 1302.59 | 0.89 | 2-S0A1 | 9.00 | 37.5 | 41.3 | 51 | 55.11 | 3.54 | 1236.80 | 0.81 | 3-S0A1 | 7.43 | 36.7 | 40.72 | 48 | 53.24 | 3.54 | 1328.86 | 0.89 | 4-S0A1 | 7.54 | 34.47 | 38.53 | 41 | 41.82 | 4.26 | 1307.77 | 0.84 | 5-S0A1 | 7.72 | 24.29 | 38.55 | 41 | 38.36 | 4.42 | 1210.54 | 0.77 |
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