International Journal of Aerospace Engineering / 2017 / Article / Tab 6

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-bench6.5924.9021.392258.200.563.883.8291288.320.88
1-S4A14.4815.6012.062849.610.852.123.6431213.570.99
2-S4A14.6612.8311.302451.830.682.363.0391108.530.91
3-S4A15.0412.9611.112254.660.602.722.8401102.850.87
4-S4A14.6213.4311.552549.960.722.253.2281168.690.97

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