International Journal of Aerospace Engineering / 2017 / Article / Tab 5

Research Article

Experimental Study of the Swirling Oxidizer Flow in HTPB/N2O Hybrid Rocket Motor

Table 5

Oxidizer mass flow rate.

Test #
(°C)

(kg/m3)

(bar)

(bar)

(g/s)

1-S4A125.0743.956.669.760.0
2-S4A126.8708.357.670.056.5
3-S4A125.8721.756.369.259.7
4-S4A126.5712.457.268.755.1

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