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Experimental solid and liquid propellant rocket development in Universiti Teknologi Malaysia: 1992-2011

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Figure

Table 1  Compositions of propellant used by Kandiah Padmanathan  4
Table 2  Nozzle configurations in Mu's experiment  6 Nozzle no  Nozzle type  Inlet
Table 3  Specification of the pressure vessel model  7
Figure 10  Observation in ballistic test for Nozzle 1 9
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