International Journal of Aerospace Engineering / 2017 / Article / Tab 2

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-S0A17.6039.243.25354.813.231302.590.89
2-S0A19.0037.541.35155.113.541236.800.81
3-S0A17.4336.740.724853.243.541328.860.89
4-S0A17.5434.4738.534141.824.261307.770.84
5-S0A17.7224.2938.554138.364.421210.540.77

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