Research Article
Experimental Study of the Swirling Oxidizer Flow in HTPB/N2O Hybrid Rocket Motor
Table 6
Ballistic characteristics of tests.
| Test # | (sec) | (bar) | (kgf) | (g/s) | (mm) | (mm/s) | O/F | (g/cm2 s) | (m/sec) | |
| 0-bench | 6.59 | 24.90 | 21.39 | 22 | 58.20 | 0.56 | 3.88 | 3.829 | 1288.32 | 0.88 | 1-S4A1 | 4.48 | 15.60 | 12.06 | 28 | 49.61 | 0.85 | 2.12 | 3.643 | 1213.57 | 0.99 | 2-S4A1 | 4.66 | 12.83 | 11.30 | 24 | 51.83 | 0.68 | 2.36 | 3.039 | 1108.53 | 0.91 | 3-S4A1 | 5.04 | 12.96 | 11.11 | 22 | 54.66 | 0.60 | 2.72 | 2.840 | 1102.85 | 0.87 | 4-S4A1 | 4.62 | 13.43 | 11.55 | 25 | 49.96 | 0.72 | 2.25 | 3.228 | 1168.69 | 0.97 |
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